Review and Editing of Unit Descriptions

ClaudeJ · Post by **ClaudeJ** » Tue Mar 12, 2024 1:54 am

Good work whacking the parasite MIM-23 description in the last update!

Weapon_671 slipped through the net.

And I would suggest to have these included in the next update:

add the Aircraft_4605.txt (#4605 - Airbus A.330-200 MRTT (UAE - 2014), and is a copy of the other A320-200 description file)
delete Aircraft_2105 (P-3AM Orion (Brazil, Navy 2012) but has the MiG-23MS description file).
delete Facility_3223 (SAM Bty Patriot but has an AN/FPS-6 Radar description file).
delete Weapon_671

CV60 · Post by **CV60** » Tue Mar 12, 2024 5:55 pm

Thanks. I'm finishing up a new update, and hopefully will get it out in the next week. I will include these changes.

CV60 · Post by **CV60** » Fri Mar 22, 2024 9:45 pm

DRAFT Rampage weapon description for comment (Weapon_3528)

OVERVIEW: The Rampage aka MARS is a long-range, solid-fuel, supersonic, air-to-ground, precision strike weapon, using GPS/INS guidance and an IIR seeker. It is with a 150 kg warhead.

DETAILS: The Rampage is intended for use in attacking high-value, well-protected targets at standoff range. It is an autonomous, stand-off weapon, capable of making quick response, precision strikes using either a pre-programmed or in-flight programed mission profile.

After launch, the missile us guided by INS and satellite. In the terminal phase, the missile uses an imaging infrared seeker. It also has a two-way datalink, allowing it to provide preliminary BDA.

Specifications:
Weight: 570 kg
Length: 4.7 m
Diameter: 0.306 m
Wingspan: ??m
Speed: 1069 knts (1980 km/hr)(M 1.6)
Range: 81-135 nm
CEP: 10.0 meters.

NOTES: IOC 2019. Used by Israel and India. Under consideration by RAF.

SOURCES: IAI. "Rampage." Accessed March 22, 2024. https://www.iai.co.il/p/rampage ; Elbit Systems. "Rampage." Accessed March 22, 2024. https://elbitsystems.com/product/rampage/.

CV60 · Post by **CV60** » Fri Aug 30, 2024 9:54 pm

DRAFT KNIFE EDGE A/B and Type 517 radar descriptions for community comment

OVERVIEW: The KNIFE REST A aka P-8 aka Dolfin is an 2-D early warning and acquisition air search radar operating in the NATO "A" band.

DETAILS: The KNIFE REST A uses a four or nine-element Yagi array mounted on a lattice mast. The oldest radar in the Soviet inventory with the strict purpose of early warning, the P-8 had limited accuracy and detection capabilities, but was inexpensive and easily maintained. While not directly capable of measuring a target's altitude, a rough altitude determination was possible using a goniometer for the phase comparison between both antenna planes.

When deployed on a 30 meter mast (called “Unzha”), which pressed the multilobe radar radiation pattern to the ground, increasing the detection range of aircraft at medium altitudes (10–16 km) became possible at distances of up to 135nm.

When deployed, the P-8 system included the “Kremnij 1” secondary radar and two electric generator trailers.

Specifications:

Frequency: 70-80 MHz (A Band (NATO), VHF Band (IEEE))
Power output: 75 kW (peak)
PRF: 90-110 pps (est., based on P-10)
Pulsewidth: 4-12 µs (est)
Range Accuracy: ??
Range: 40-81nm

On/Off time: ??

NOTES: IOC 1952.

SOURCES: NATO, "Current Soviet Block Equipment: Landbased" (12 February 1968) at page 1-A-19 ; Pike, John. "KNIFE REST." GlobalSecurity.org. Last modified 8, 2019. https://www.globalsecurity.org/military ... e-rest.htm. ;"SOV - P-10 (." Armedconflicts.com. Accessed August 29, 2024. https://www.armedconflicts.com/SOV-P-10 ... -RL-t37633. ;"Type 517M - Radartutorial." Grundlagen Der Radartechnik. Accessed August 29, 2024. https://www.radartutorial.eu/19.kartei/ ... 36.en.html.

---------------------------------------------------------------------------
OVERVIEW: The KNIFE REST A aka P-8 aka Dolfin is an 2-D early warning and acquisition air search radar operating in the NATO "A" band.

DETAILS: The KNIFE REST A uses a four or nine-element Yagi array mounted on a lattice mast. The oldest radar in the Soviet inventory with the strict purpose of early warning, the P-8 had limited accuracy and detection capabilities, but was inexpensive and easily maintained. While not directly capable of measuring a target's altitude, a rough altitude determination was possible using a goniometer for the phase comparison between both antenna planes.

When deployed on a 30 meter mast (called “Unzha”), which pressed the multilobe radar radiation pattern to the ground, increasing the detection range of aircraft at medium altitudes (10–16 km) became possible at distances of up to 135nm.

When deployed, the P-8 system included the “Kremnij 1” secondary radar and two electric generator trailers.

Specifications:

Frequency: 70-80 MHz (A Band (NATO), VHF Band (IEEE))
Power output: 75 kW (peak)
PRF: 90-110 pps (est., based on P-10)
Pulsewidth: 4-12 µs (est)
Range Accuracy: ??
Range: 40-81nm

On/Off time: ??

NOTES: IOC 1952.

SOURCES: NATO, "Current Soviet Block Equipment: Landbased" (12 February 1968) at page 1-A-19 ; Pike, John. "KNIFE REST." GlobalSecurity.org. Last modified 8, 2019. https://www.globalsecurity.org/military ... e-rest.htm. ;"SOV - P-10 (." Armedconflicts.com. Accessed August 29, 2024. https://www.armedconflicts.com/SOV-P-10 ... -RL-t37633. ;"Type 517M - Radartutorial." Grundlagen Der Radartechnik. Accessed August 29, 2024. https://www.radartutorial.eu/19.kartei/ ... 36.en.html.
----------------------------------------------------------------------------------------------------------------
OVERVIEW: The Type 517 is a shipboard 2-D early warning and acquisition air search radar operating in the NATO "A" band.

DETAILS: The Type 517 radar is used on larger ships of the Chinese Navy. It is very similar to the Russian Knife Rest B Radar, using a similar Yagi-Uda array, it has much more modern electronics. It is capable of tracking more than 20 targets. Because of the long wavelength, the radar has anti-stealth and Anti-ARM (anti-radiation missile) attack capabilities.

Specifications:

Frequency: 180-210 MHz (A Band (NATO), VHF Band (IEEE))
Power output: 25 kW (peak)
PRF: 50-100 pps
Pulse width: 4-12 µs
Accuracy: 200 meters (range); 1° (azimuth)
Range:
4m2 RCS: 189nm
0.1m2 RCS: 54nm

NOTES: IOC 1952. The Type 517 is a very similar to the Knife Rest B. The radar has been significantly updated for use against stealth aircraft.

SOURCES: NATO, "Current Soviet Block Equipment: Landbased" (12 February 1968) at page 1-A-19 ; Pike, John. "KNIFE REST." GlobalSecurity.org. Last modified 8, 2019. https://www.globalsecurity.org/military ... e-rest.htm. ;"SOV - P-10 (." Armedconflicts.com. Accessed August 29, 2024. https://www.armedconflicts.com/SOV-P-10 ... -RL-t37633. ;"Type 517M - Radartutorial." Grundlagen Der Radartechnik. Accessed August 29, 2024. https://www.radartutorial.eu/19.kartei/ ... 36.en.html ; Jane's Radar and Electronic Warfare Systems, 2002-03, "P-10 early warning radar", 02 July 2001 ; "Type 517 Radar." Wikipedia, the Free Encyclopedia. Last modified December 25, 2022. https://en.wikipedia.org/wiki/Type_517_radar ; Tracey, Mrs. "High Accuracy Air / Land Surveillance Radar System Of Long Range Detection." Quality Electro Optical Tracking System & Electro Optical Sensor System Factory from China. Accessed August 30, 2024. https://www.eo-irsystems.com/sale-78386 ... ction.html.

CV60 · Post by **CV60** » Sat Aug 31, 2024 10:27 pm

DRAFT BAND STAND radar description for comment

OVERVIEW: The BAND STAND aka MR 331 Mineral-ME is a shipborne 2-D, multifunctional radar and missile tracking system with OtH capability operating in the I band (active) and the I, G, E/F and D bands (passive) (NATO).

DETAILS: The Mineral-ME/BAND STAND is a shipborne multifunctional surface search radar intended for medium and large displacement surface fighting ships and is used for surface surveillance and SSM missile targeting. The Mineral-ME system consists of three modular antennas: Mineral-ME1 active radar; Mineral-ME2 passive receiver; and the Mineral-МЕЗ data exchange and orientation datalink. The active radar provides OtH detection, location, tracking, classification of surface targets, and features a troposcatter antenna back-to-back with a II band ducting antenna. The passive radar provides OtH radar detection, classification, and target designation. Finally, the data exchange antenna (LIGHT BULB) provides for data exchange between up to nine compatible remote sensor platforms.

The active radar can track up to thirty contacts and designating up to ten targets. The system can exchange data with up to 9 surface ships.

Specifications:

Frequency (active): 8-10 GHz (I Band (NATO), X Band (IEEE))
Power output: ?? kW(average); ?? MW (peak)
PRF: ?? pps (avg)
Pulsewidth: ?? µs
Range Accuracy: 50 meters (active); 10% range (passive)
Range: 135nm max surface detection range (active)
16nm (weapon guidance datalink)
242 nm (max passive)

NOTES: IOC 1999. This radar system was selected to detect surface targets onboard the cancelled Project 21956 Russian fourth generation destroyer. Other applications of the Mineral Radar are the Project 22800 class corvettes and Udaloy class destroyers. Mineral-ME is the export version, and Mineral is the domestic Soviet/Russian version of the system.

SOURCES: "Mineral-ME." Guide to Military Equipment and Civil Aviation. Last modified March 15, 2018. https://www.deagel.com/Components/Mineral-ME/a002366. ; "Shipborne Multifunctional Radar System Mineral-ME | Catalog Rosoboronexport." Рособоронэкспорт | Официальный сайт. Accessed August 31, 2024. https://roe.ru/eng/catalog/naval-system ... ineral-me/. ; Friedman, Norman. The Naval Institute Guide to World Naval Weapon Systems. Annapolis, MD: US Naval Institute Press, 2006., pg. 222.

CV60 · Post by **CV60** » Mon Sep 02, 2024 7:16 pm

DRAFT CROSS ROUND radar description for public edit/comment

OVERVIEW: The CROSS ROUND aka MR352 Pozitive-ME1.2 is a shipborne 3-D, air and surface search and target designation radar operating in the I/J band (active) (NATO).

DETAILS: The CROSS ROUND uses a planar array antenna using phase/frequency scanning, with an IFF antenna along its lower edges. It features a high-speed rotation and electronic elevation scanning, to provide a short reaction time, high throughput capacity and target designation capability. It is capable of tracking up to 40 targets simultaneiously, and can lock onto a designated target in 3.5 seconds.

Specifications:

Frequency (active): 8-12 GHz (I/J Band (NATO), X Band (IEEE))
Power output: 45 kW (peak)
PRF: ?? pps (avg)
Pulsewidth: ?? µs
Range: 43nm max; 63,300 feet (altitude)
Detection:
1m² RCS 27nm@1000m altitude
0.031m² RCS: 7.0nm@15m altitude
10000m² RCS: 0.9-0.95% radar horizon
Accuracy: 20-40m (range); 0.16° (azimuth and elevation)
On/off time: 3 min.

NOTES: IOC 1999. Users: China, Algeria

SOURCES: "Family Active Radars Pozitiv-ME1 | Catalog Rosoboronexport." Рособоронэкспорт | Официальный сайт. Accessed September 2, 2024. https://roe.ru/eng/catalog/naval-system ... ozitiv-me/ and https://roe.ru/esp/catalog/marina-de-gu ... tiv-me1-2/ ; Friedman, Norman. The Naval Institute Guide to World Naval Weapon Systems. Annapolis, MD: US Naval Institute Press, 2006., pg. 273-74.

CV60 · Post by **CV60** » Thu Sep 19, 2024 8:04 pm

DRAFT AN/SPS-48E description for comment

OVERVIEW: The AN/SPS-48E NTU (New Threat Upgrade) is a long-range, 3-D, phased array air search radar operating in the NATO E/F bands.

DETAILS: The AN/SPS-48E is a frequency-scanning radar using pencil beams. The NTU modifications also include a low sidelobe antenna, allowing it to operate under heavy jamming conditions.

The SPS-48E radar is mechanically scanned in azimuth and is frequency scanned in elevation. Frequency steering permits the use of multiple simultaneous elevation beams. Each elevation beam has a different frequency, and each frequency uses a separate receiver channel. This feature allows the radar to cover the entire search volume with narrow pencil beams in a short time. By utilizing nine simultaneous beams in a beam group with a separate receiver for each, the radar can illuminate the entire long-range/high elevation angle coverage volume required, achieve good azimuth and elevation accuracy with multiple pencil beams, and maintain the 4-s antenna rotation rate. The radar can track hundreds of aircraft simultaneously.

The SPS-48 uses Doppler waveforms coupled with image processing algorithms to provide very fast detection of low-flying threats as they cross the radar horizon. The radar has demonstrated superior detection and tracking of high and low altitude cruise missiles, supersonic aircraft at all altitudes, and helicopters.

The SPS-48E is a “plug and play” system, allowing it to easily integrate into other C4I systems. It can provide properly formatted track data to all modern weapons systems, including the Patriot and the Improved Hawk, SM-2, ESSM and RAM. Furthermore, it can accept and execute commands from external air defense or shipboard combat systems.

Specifications:

Frequency (active): 2.9-3.1 GHz (E/F Band (NATO), S Band (IEEE))
Power output: 2.4 MW (peak); 35 kW (average)
PRF: 330-2250; 1250-2000 pps (avg)
Pulsewidth: 3 µs per beam; 27 total
Range: 215nm (instrumented)
Detection:
5m² RCS 220 nm
1m² RCS 125 nm
0.1m² RCS 17 nm (at low altitude)
Resolution: 476 m (range); 0.16° ( elevation)
On/off time: snap on/off

NOTES: IOC 1987. Although most units are shipborne, some have been installed at land bases in CONUS.

SOURCES: Friedman, Norman. The Naval Institute Guide to World Naval Weapon Systems. Annapolis, MD: US Naval Institute Press, 2006., pg. 312 ; Jane's Radar and Electronic Warfare Systems 2002-03, "ANSPS-48E air surveillance radar, 08 August 2001; Roulette and Skrivseth, "Coherent Data Collection and Analysis Capability for the AN/SPS-48E Radar," John Hopkins APL Technical Digest, vol 18, No. 3 (1997); Forecast International, "SPS-48E"; AN/SPS-48E - Radartutorial. (n.d.). Grundlagen der Radartechnik. https://www.radartutorial.eu/19.kartei/ ... 10.en.html ;
An/sps-48e. (2022, January 26). Guide to Military Equipment and Civil Aviation. https://www.deagel.com/Components/ANSPS-48E/a001681

CV60 · Post by **CV60** » Thu Sep 19, 2024 10:17 pm

OVERVIEW: The AN/SPQ-9B aka "spook nine" is a short-range, pulse-Doppler, 2-D, surface search and fire control radar operating in the NATO I band.

DETAILS: The AN/SPQ-9B is an I-Band, pulse Doppler, frequency agile radar designed specifically for the littoral environment. The radar scans out to the horizon and performs simultaneous and automatic air and surface target detection and tracking of low flying subsonic and supersonic ASCMs, surface threats and low/slow flying aircraft, UAVs and helicopters. It has a very high clutter improvement factor supporting a very low false track rate in the littorals and in high clutter environments.

The AN/SPQ-9B antenna provides for three beams. If an air target is detected in the main beam, two look-back beams provide confirmation and track promotion resulting in “single-scan track” disclosure to a ship’s weapon system.

Specifications:

Frequency (active): 8-12.5 GHz (I Band (NATO), X Band (IEEE))
Power output: 18 kW (peak);
PRF: 3000 pps (avg)
Pulsewidth: 0.1-8 µs
Range: 25 nm (est)
Detection:

Resolution: ??
On/off time: ??

NOTES: IOC 2001

SOURCES: Friedman, Norman. The Naval Institute Guide to World Naval Weapon Systems. Annapolis, MD: US Naval Institute Press, 2006., pg. 322-3 ; Jane's Radar and Electronic Warfare Systems 2002-03, "AN/SPQ-9B air surveillance radar, 04 March 2002; "AN/SPQ-9B - Radartutorial." Grundlagen Der Radartechnik. Accessed September 19, 2024. https://www.radartutorial.eu/19.kartei/ ... 01.en.html. ; "AN/SPQ-9B Radar Set." United States Navy. Last modified November 15, 2021. https://www.navy.mil/Resources/Fact-Fil ... radar-set/.

Rams128 · Post by **Rams128** » Fri May 30, 2025 12:58 am

AIM-120's AMRAAM missiles

-----AIM-120A AMRAAM || Weapon_1383----------

OVERVIEW: The AIM-120A AMRAAM is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile.

DETAILS: The AIM-120A was the first operational AMRAAM (Advanced Medium-Range Air-to-Air Missile), designed to replace the AIM-7 Sparrow with a fire-and-forget missile featuring active radar homing and mid-course datalink updates. It used a 23 kg blast-fragmentation warhead and could engage multiple targets simultaneously at up to 50 km range, depending on launch conditions. Highly maneuverable and equipped with ECCM, it offered improved survivability in contested environments and set a new standard for autonomous air-to-air combat.

SPECIFICATIONS:
Guidance: Inertial + mid-course datalink + active radar homing (WGU-16/B)
Warhead: 23 kg WDU-33/B blast-fragmentation with proximity fuse
Propulsion: WPU-6/B solid-fuel rocket motor
Range: ~27 nm (50 km) (depending on launch altitude and speed)
Speed: Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: 0.53 m
Weight: ~158 kg
Platforms: F-15, F-16, F/A-18, F-4, F-14 (limited), Eurofighter (test), Mirage 2000

NOTES:
Initial Operational Capability (IOC): 1991 (USAF)
Operators: United States, United Kingdom, Germany, Norway, Denmark, Turkey, Greece, Saudi Arabia, Israel, Taiwan, Japan, South Korea, Singapore, Egypt, Jordan, UAE, Australia, Thailand, Chile, Portugal, Spain, Italy, Netherlands, and others
Conflict Use: Used during Operation Southern Watch (Iraq), Operation Deny Flight (Bosnia), and later variants evolved from AIM-120A saw widespread use in Kosovo, Iraq (2003), and Syria.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
Raytheon AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
Federation of American Scientists: https://man.fas.org/dod-101/sys/missile/aim-120.htm
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Jane's Air-Launched Weapons (subscription)
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120B AMRAAM || Weapon_446----------

OVERVIEW: The AIM-120B AMRAAM is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile..

DETAILS: The AIM-120B retained the same aerodynamic design and performance envelope as the AIM-120A but added a modular guidance section with a digital processor and reprogrammable software. This allowed the missile to be updated with new threat data and software enhancements without opening the guidance section, improving lifecycle efficiency and battlefield adaptability. with a 23 kg blast-fragmentation warhead, Its all-weather, active radar seeker enables autonomous terminal homing after mid-course guidance via inertial navigation and datalink. It remained a key medium-range missile in U.S. and allied inventories well into the 2010s.

SPECIFICATIONS:
Guidance: Inertial + mid-course datalink, active radar terminal homing
Warhead: 23 kg high-explosive blast-fragmentation (WDU-33/B)
Range: ~27 nm (50 km) (varies with launch conditions)
Speed: ~Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: 0.64 m
Weight: ~158 kg
Platforms: F-15, F-16, F/A-18, Eurofighter Typhoon, F-4, Gripen, and others

NOTES:
Initial Operational Capability (IOC): ~1995
Operators: United States, Norway, United Kingdom, Germany, Japan, South Korea, Turkey, Greece, Spain, Egypt, Netherlands, Portugal, Saudi Arabia, UAE, Taiwan, Singapore, Poland, and others
Interesting Fact: The AIM-120B’s modular electronics made it the first AMRAAM variant to allow depot-level reprogramming, significantly streamlining upgrades and maintenance.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
U.S. Department of Defense (DoD) budget documents and fact sheets
Raytheon – AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
SIPRI Arms Transfers Database
Federation of American Scientists (FAS) – AMRAAM Profile
Jane’s Air-Launched Weapons (IHS Markit, subscription)
RAND Corporation – Analysis of Air Combat Effectiveness Reports
Congressional Research Service (CRS) – AMRAAM Overview
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

----- AIM-120C AMRAAM P3I || Weapon_946----------

OVERVIEW: The AIM-120C AMRAAM P3I Phase 1 is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile.

DETAILS: Part of the Pre-Planned Product Improvement (P3I) Phase 1, with a 23 kg blast-fragmentation warhead, the AIM-120C marked the third major evolution in the AMRAAM series. The main change from earlier models was the redesign of the missile’s fins and control surfaces specifically clipped wings and fins to allow internal storage in stealth aircraft such as the F-22 Raptor. It retained the WPU-6/B solid-fuel rocket motor and WDU-33/B warhead, but included enhancements in its guidance section, notably the WGU-44/B, which provided improved electronic counter-countermeasures (ECCM) and better target discrimination in dense threat environments.

SPECIFICATIONS:
Guidance: Inertial + mid-course datalink, active radar terminal homing (WGU-44/B)
Warhead: 23 kg high-explosive blast-fragmentation (WDU-33/B)
Range: ~27 nm (50 km) (varies with altitude and launch speed)
Speed: ~Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: ~0.45 m (clipped for internal carriage)
Weight: ~158 kg
Platforms: F-15, F-16, F/A-18, F-22, Eurofighter Typhoon, Gripen, and others

NOTES:
Initial Operational Capability (IOC): ~1999
Operators: United States, United Kingdom, Germany, Japan, Turkey, Norway, Greece, Denmark, South Korea, Israel, Saudi Arabia, UAE, Australia, Singapore, and others
Interesting Fact: The AIM-120C was the first AMRAAM variant designed specifically with stealth platform integration in mind, optimizing its form factor for internal weapons bays.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
Raytheon – AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
Federation of American Scientists: https://man.fas.org/dod-101/sys/missile/aim-120.htm
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Jane's Air-Launched Weapons (subscription)
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120C-4 AMRAAM P3I.2 || Weapon_53----------

OVERVIEW: The AIM-120C-4 AMRAAM is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile, upgraded under the P3I Phase 2 program for enhanced ECCM and lethality.

DETAILS: The AIM-120C-4 was part of the Phase 2 upgrade in the AMRAAM Pre-Planned Product Improvement (P3I.2) program. with a 23 kg blast-fragmentation warhead, It featured internal enhancements aimed at improving effectiveness in electronically contested environments. These included upgraded electronic counter-countermeasures (ECCM), improved mid-course datalink guidance, and a refined active radar seeker for superior terminal tracking. The missile maintained the clipped-fin design introduced in the AIM-120C for compatibility with internal bays of stealth aircraft such as the F-22 Raptor. Its electronics improvements enabled better performance against maneuvering targets and radar jamming techniques.

SPECIFICATIONS:
Guidance: Inertial + mid-course datalink, active radar terminal homing
Warhead: 23 kg high-explosive blast-fragmentation (WDU-33/B)
Range: ~27 nm (50 km) (approximate, varies with launch profile)
Speed: ~Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: ~0.45 m
Weight: ~158 kg
Guidance System: Inertial Navigation System (INS) with mid-course updates via datalink and Active radar homing for terminal guidance
Platforms: F-15, F-16, F/A-18, F-22, Eurofighter Typhoon, Gripen, and others

NOTES:
Initial Operational Capability (IOC): ~2001
Operators: United States, Japan, South Korea, Singapore, Israel, Saudi Arabia, Australia, Greece, Turkey, and other
Interesting Fact: The C-4 served as an interim capability bridging the gap between earlier C-variants and the more capable C-5 with increased kinematic range.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
Raytheon AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
Federation of American Scientists: https://man.fas.org/dod-101/sys/missile/aim-120.htm
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Jane's Air-Launched Weapons (subscription)
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120C-5 AMRAAM P3I.2 || Weapon_897----------

OVERVIEW: The AIM-120C-5 AMRAAM is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile, introduced under the P3I Phase 2 program with extended range and improved electronic counter-countermeasures.

DETAILS: The AIM-120C-5 was the second and final missile developed under the P3I.2 effort. with an 18–20 kg blast-fragmentation warhead, It retained the clipped-fin design of earlier C-models for internal carriage compatibility with stealth aircraft like the F-22. The most notable physical upgrade was the adoption of the WPU-16/B “large-grain” solid-propellant rocket motor, which was approximately 12 cm longer than previous motors and significantly increased the missile's kinematic performance. It also included a shortened WCU-28/B control section to accommodate the longer motor. Internally, it carried forward the modular electronics, WGU-44/B seeker, and advanced ECCM software from previous variants, enabling better survivability in jamming environments.

SPECIFICATIONS:
Guidance: Inertial with mid-course datalink; active radar terminal homing
Warhead: 18–20 kg WDU-41/B blast-fragmentation with proximity/impact fuze
Range: ~56nm (105 km) (approximate, depending on launch conditions)
Speed: ~Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: ~0.45 m
Weight: ~162 kg
Platforms: F-15, F-16, F/A-18, F-22, Typhoon, Gripen, others

NOTES:
Initial Operational Capability (IOC): ~2003
Operators: United States, Australia, Saudi Arabia, Japan, South Korea, Singapore, Norway, Poland, Israel, Finland, United Kingdom, and others
Fact: The AIM-120C-5 marked a significant step forward in range and lethality, becoming the most widely exported and fielded AMRAAM variant during the 2000s.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
Raytheon AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
Federation of American Scientists: https://man.fas.org/dod-101/sys/missile/aim-120.htm
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Jane's Air-Launched Weapons (subscription)
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120C-6 AMRAAM P3I.2 || Weapon_52----------

OVERVIEW: The AIM-120C-6 AMRAAM is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile.

DETAILS: The AIM-120C-6 was a refinement of the AIM-120C-5 under the continued Phase 2 P3I effort. with an 18–20 kg blast-fragmentation warhead, it retained the same aerodynamic structure, solid-fuel WPU-16/B motor, and guidance system as the C-5 variant, its key improvement was a redesigned Target Detection Device (TDD). The updated TDD offered improved reliability in target acquisition and engagement, particularly under electronic warfare conditions or cluttered environments. This minor but important upgrade enhanced the missile’s kill probability and reduced the chances of failed engagements due to proximity fuze issues.

SPECIFICATIONS:
Guidance: Inertial with mid-course datalink; active radar terminal homing
Warhead: 18–20 kg WDU-41/B blast-fragmentation with improved proximity/impact fuze
Range: ~57nm (105 km) (approximate, subject to launch parameters)
Speed: ~Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: ~0.45 m
Weight: ~162 kg
Platforms: F-15, F-16, F/A-18, F-22, Eurofighter Typhoon, Gripen, others

NOTES:
Initial Operational Capability (IOC): ~2005
Operators: United States, Saudi Arabia, Japan, Singapore, South Korea, Poland, Norway, Finland, and others
The AIM-120C-6 introduced no external changes over the C-5 but internally addressed reliability gaps in terminal engagement by modernizing its fuzing system.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
U.S. Department of Defense (DoD) budget documents and fact sheets
Raytheon – AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
SIPRI Arms Transfers Database
Federation of American Scientists (FAS) – AMRAAM Profile
Jane’s Air-Launched Weapons (IHS Markit, subscription)
RAND Corporation – Analysis of Air Combat Effectiveness Reports
Congressional Research Service (CRS) – AMRAAM Overview
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120C-7 AMRAAM P3I.3 || Weapon_718----------

OVERVIEW: The AIM-120C-7 AMRAAM is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile, featuring major enhancements in guidance, range, and electronic counter-countermeasures (ECCM).

DETAILS: the AIM-120C-7 marked a significant step forward in the AMRAAM family under the Phase 3 Increment 3 (P3I.3) effort. Key upgrades included enhanced guidance algorithms, a more advanced active radar seeker, and improved datalink functionality for more accurate mid-course updates. These changes allowed the missile to operate more effectively in high-electronic-warfare (EW) environments and extended its no-escape and engagement envelopes. With an 18–20 kg blast-fragmentation warhead, the C-7 maintained the clipped-fin design of the C-series, ensuring compatibility with internal bays of stealth fighters like the F-22 Raptor.

SPECIFICATIONS:
Guidance: Inertial + mid-course datalink; active radar terminal homing
Warhead: 18–20 kg WDU-41/B blast-fragmentation with FZU-49/B proximity/impact fuze
Range: ~65nm (120 km) (estimated; highly dependent on launch parameters)
Speed: ~Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: ~0.45 m
Weight: ~162 kg
Platforms: F-15, F-16, F/A-18, F-22, F-35 (external carriage), Eurofighter Typhoon, Gripen, Rafale (via NATO standard integration), and others

NOTES:
Initial Operational Capability (IOC): 2008
Operators: United States, Australia, Belgium, Canada, Chile, Denmark, Finland, Germany, Greece, Indonesia, Israel, Japan, Jordan, Kuwait, Morocco, Netherlands, Norway, Oman, Poland, Portugal, Qatar, Romania, Saudi Arabia, Singapore, Slovakia, South Korea, Spain, Sweden, Taiwan, Thailand, Turkey, United Arab Emirates, United Kingdom
Fact: The C-7 version was developed in part to address challenges posed by advanced enemy electronic warfare systems and agile air targets emerging in the early 21st century.
This version was widely exported and became the backbone of many allied air forces’ BVR capabilities, thanks to its performance, reliability, and integration with a broad range of Western and NATO-standard platforms.

SOURCES:
UNCLASSIFIED Selected Acquisition Report (SAR) 2018 and 2014: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf || https://www.esd.whs.mil/Portals/54/Docu ... c_2014.PDF
U.S. Department of Defense (DoD) budget documents and fact sheets
Raytheon – AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
SIPRI Arms Transfers Database
Federation of American Scientists (FAS) – AMRAAM Profile
Jane’s Air-Launched Weapons (IHS Markit, subscription)
RAND Corporation – Analysis of Air Combat Effectiveness Reports
Congressional Research Service (CRS) – AMRAAM Overview
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120D AMRAAM P3I.4 (AIM-120C-8) || Weapon_51----------

OVERVIEW: The AIM-120D AMRAAM (also designated AIM-120C-8) is a beyond-visual-range, fire-and-forget, active radar-guided air-to-air missile with datalink capability.

DETAILS: Entering service in the early 2010s, the AIM-120D represents the most advanced variant of the AMRAAM family. Developed as part of the P3I Phase 4 upgrade, with an 18–20 kg blast-fragmentation warhead, major enhancements to range and accuracy, the D-model features significant software and hardware improvements over earlier variants. These include a two-way datalink for in-flight targeting updates, an upgraded GPS-assisted inertial navigation system, and enhanced kinematic performance. Its seeker boasts refined signal processing for better target discrimination and ECCM performance in contested environments.

The missile retains the clipped-fin design for compatibility with internal weapons bays of stealth aircraft like the F-22 and F-35. It offers an extended maximum range and a larger no-escape zone compared to previous versions, significantly increasing pilot survivability and lethality in modern air combat.

SPECIFICATIONS:
Guidance: Inertial + GPS-aided mid-course guidance; two-way datalink; active radar terminal homing
Warhead: 18–20 kg WDU-41/B blast-fragmentation with FZU-49/B proximity/impact fuze
Range: ~86nm (160 km) (estimated, exact classified)
Speed: Mach 4
Length: 3.66 m
Diameter: 178 mm
Wingspan: ~0.45 m
Weight: ~162 kg
Platforms: F-15, F-16, F/A-18, F-22, F-35, Eurofighter Typhoon, Gripen (via integration), and others

NOTES:
Initial Operational Capability (IOC): 2015
Operators: United States, Australia, Japan, South Korea, Poland, Norway, United Kingdom, Denmark, Saudi Arabia, Singapore, Qatar, Spain, Switzerland, Netherlands, Finland, Canada, Romania
Interesting Fact: The AIM-120D’s two-way datalink allows real-time communication with the launch platform, enabling retargeting and engagement flexibility mid-flight an unprecedented capability among legacy AMRAAMs.

SOURCES:
Raytheon – AMRAAM Datasheet (Archived)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
Federation of American Scientists: https://man.fas.org/dod-101/sys/missile/aim-120.htm
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
UNCLASSIFIED Selected Acquisition Report (SAR) 2018: https://www.esd.whs.mil/Portals/54/Docu ... c_2018.pdf
Jane's Air-Launched Weapons (subscription)
Army Recognition Group Magazine: https://www.armyrecognition.com/militar ... ir-missile
https://www.deagel.com/Weapons/AIM-120%20AMRAAM/a001164
https://en.missilery.info/missile/aim120

-----AIM-120D-3 AMRAAM F3R (AIM-120C-8)|| Weapon_4290----------

OVERVIEW: The AIM-120D F3R is a long-range, active radar-guided, air-to-air missile with upgraded software and guidance systems for improved range, accuracy, and ECM resistance.

DETAILS: Also known as the AIM-120C-8 SIP (Software Improvement Program), the D-3 refresh resolves guidance-section obsolescence with 15 new circuit cards and a model-based, open-architecture processor. Key gains are: a more powerful GPS-aided INS, refined seeker algorithms for better ECCM and target discrimination, and a 50 % range/no-escape-zone growth over AIM-120C-7. The clipped-fin airframe is unchanged, preserving internal-bay carriage on F-22 and F-35 while remaining compatible with legacy fighters.

SPECIFICATIONS:
Guidance: Inertial + GPS-aided mid-course; two-way datalink; active-radar terminal seeker
Warhead: 18–20 kg WDU-41/B blast-fragmentation with FZU-49/B proximity/impact fuze
Range: ~95 nm (175 km) (estimated, classified)
Speed: ≈Mach 4
Length: 3.66
Diameter: 178 mm
Wingspan: 0.45 m
Weight: ~162 kg
Platforms: F-15, F-16, F/A-18, F-15EX, F-22, F-35, Eurofighter Typhoon, Gripen, and other AMRAAM-integrated aircraft.

NOTES:
Initial Operational Capability (IOC): 2024 (USAF & USN)
Operators (ordered or fielding): United States, Australia, Japan, Netherlands, Poland, Norway, Denmark, Finland, Saudi Arabia, Spain, Qatar, Canada, Romania and others via Foreign Military Sales.
Interesting Fact: The F3R guidance section’s open-architecture cards can be re-programmed in the field, allowing smartphone-style software drops that add new capabilities without touching hardware.

SOURCES:
RTX press release “Most advanced AMRAAM variant, AIM-120D-3, completes critical milestone” (Apr 18 2023)
DOT&E FY2024 Annual Report, AMRAAM AIM-120D-3 SIP-3F fielding note (Feb 2025)
Janes, “Australia seeks to procure new AIM-120C-8/D-3 missiles” (Apr 10 2025)
Army Recognition, “Netherlands orders AIM-120D-3 for F-35 fleet” (Dec 6 2024)
Airforce-Technology, AIM-120 AMRAAM factfile (May 2025)
DefenceSecurityAsia, “U.S. to sell AIM-120D-3/C-8 missiles to Japan” (Jan 2025)
Official United States Air Force Website: https://www.af.mil/News/Article-Display ... 20-amraam/
Federation of American Scientists: https://man.fas.org/dod-101/sys/missile/aim-120.htm

______________________________________________________________________________________________________________________________________________________________________________________________________________________

Rams128 · Post by **Rams128** » Sat May 31, 2025 1:44 am

Python's Missiles

-----Shafrir 2 || Weapon_1745----------

OVERVIEW: The Shafrir 2 is an Israeli short-range, infrared-guided, fire-and-forget air-to-air missile with an 11 kg blast-fragmentation warhead and an effective engagement range of roughly 5–7 km.

DETAILS: Developed by Rafael and fielded in 1971, Shafrir 2 replaced the limited-production Shafrir 1 and gave the Israeli Air Force a competitive dog-fight missile before the 1973 Yom Kippur War. It uses an improved all-aspect* passive IR seeker, a larger HE-fragmentation warhead, and a more energetic solid-fuel rocket motor than its predecessor. The missile can be slaved to the aircraft radar or cued visually; once fired it homes autonomously on the target’s heat signature. Although later eclipsed by the Python series, Shafrir 2 proved effective in Middle-East conflicts and was exported to several nations for Mirage III/5, Nesher/Dagger, Kfir and F-5 platforms.

*Practical off-boresight was limited compared with modern HOBS designs, but the seeker could engage front-hemisphere targets under favourable aspects.

SPECIFICATIONS:
Guidance: Passive infrared homing (all-aspect)
Warhead: 11 kg HE blast-fragmentation (proximity / impact fuze)
Range: 0.5 km (min) ≈ 7 km (max)
Speed: ~Mach 2.5–2.9
Length: 2.50 m
Diameter: 160 mm
Wingspan: 0.66 m
Weight: 93 kg
Platforms: Mirage III/5 & derivatives, Kfir/Nesher, F-4E, F-5E, A-4 variants

NOTES:
Initial Operational Capability (IOC): 1971
Operators: Israel, Argentina, Ecuador, Colombia, Chile, South Africa, Singapore, Venezuela
Combat use: Extensively employed by Israel in the 1973 Yom Kippur War (credited with dozens of kills) and by Argentina during the 1982 Falklands/Malvinas War.
Interesting fact: Shafrir 2’s seeker and airframe formed the engineering baseline for Rafael’s later Python-3, illustrating the evolutionary path of Israeli short-range AAMs.

SOURCES:
Rafael Advanced Defense Systems: https://www.rafael.co.il/
Jane’s Air-Launched Weapons: Various editions
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/row/shafrir.htm
SIPRI Arms Transfers Database: https://armstrade.sipri.org
Y. Bar-Siman-Tov, War of Attrition & Yom Kippur War Air Combat Analysis: (Published by the IAF Historical Archives)
Argentine Air Force After-Action Reports (1982): Archival materials referenced in declassified conflict assessments and post-conflict analysis publications

-----Python 3 || Weapon_1749 ----------

OVERVIEW: The Python 3 is a short-range, infrared-guided air-to-air missile developed by Israel with a high-explosive fragmentation warhead and a range of approximately 15 km.

DETAILS: A significant improvement over the Shafrir 2, the Python 3 introduced all-aspect engagement, allowing lock-on before and after launch from any angle. It featured an upgraded seeker with improved counter-countermeasures and a higher off-boresight capability, enhancing effectiveness in close-range aerial combat.
Its aerodynamic design provided excellent maneuverability, making it a competitive dogfighting missile in the late Cold War era. Python 3 was widely exported and became a standard in many air forces’ short-range missile inventories.

SPECIFICATIONS:
Guidance: Infrared homing (passive)
Warhead: 11 kg high-explosive fragmentation
Range: ~ 15 km
Speed: ~ Mach 2
Length: 3 m
Diameter: 160 mm
Wingspan: 0.86 m
Weight: 120 kg
Platforms: Kfir, F-4 Phantom II, F-5, F-16, Mirage III/5, IAI Nesher, and others

NOTES:
Initial Operational Capability (IOC): 1978
Operators: Israel, Chile, Colombia, Ecuador, El Salvador, Singapore, South Africa, Sri Lanka, Thailand, Venezuela
Combat Use: Used extensively by the Israeli Air Force during the 1982 Lebanon War, reportedly achieving a high kill rate in dogfights against Syrian aircraft.

SOURCES:
Rafael Advanced Defense Systems (archived materials)
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Jane’s Air-Launched Weapons (IHS Markit)
Federation of American Scientists (FAS) – Python Missile Series
GlobalSecurity.org – Python 3
RAND Corporation – "The Air War in Lebanon, 1982"
Weaponsystems.net: https://weaponsystems.net/system/1194-Python%203
Wikipedia: https://en.wikipedia.org/wiki/Python_(missile)
SA Air Force: https://www.saairforce.co.za/the-airfor ... l-python-3

-----Python 4 || Weapon_1050----------

OVERVIEW: The Python 4 is a fourth-generation, short-range, infrared-guided air-to-air missile featuring an 11 kg blast-fragmentation warhead and a maximum range of up to 18 km.

DETAILS: Developed by Israel's Rafael Advanced Defense Systems, the Python 4 entered service in the early 1990s as a successor to the Python 3. It introduced significant advancements, including a dual-band infrared seeker with high off-boresight capability, allowing engagements at angles up to 60 degrees from the aircraft's axis. The missile is compatible with helmet-mounted sight systems, such as Elbit Systems' DASH, enabling pilots to lock onto targets by simply looking at them. Its high maneuverability, achieved through aerodynamic design and thrust vector control, allows it to perform high-G turns, making it effective in close-combat scenarios. The Python-4 also features advanced infrared counter-countermeasures (IRCCM) to resist enemy flares and other decoys.

SPECIFICATIONS:
Length: 3.0 m
Diameter: 160 mm
Wingspan: 0.64 m / 640 mm
Weight: 105 kg
Warhead: 11 kg high-explosive blast-fragmentation
Guidance: Dual-band infrared homing with IRCCM
Speed: ~ Mach 2
Range: 18 km (max)

NOTES:
Initial Operational Capability (IOC): 1993
Platforms: F-15, F-16, F-5, Mirage III, Mirage 5, Kfir, JAS 39 Gripen, HAL Tejas, and others
Operators: Israel, India, Brazil, Chile, Colombia, Ecuador, Georgia, Peru, Singapore, South Africa, Thailand, Vietnam

SOURCES:
Rafael Advanced Defense Systems: https://www.rafael.co.il/worlds/air/air ... /python-4/
GlobalSecurity: https://www.globalsecurity.org/military ... ython4.htm
Air Power Australia: https://www.ausairpower.net/TE-Gen-4-AAM-97.html
Wikipedia: https://en.wikipedia.org/wiki/Python_(missile)
FlightGlobal: https://www.flightglobal.com/mdc-to-tes ... 36.article

----- Python 5|| Weapon_516 ----------

OVERVIEW: The Python 5 is a short-to-medium-range, fifth-generation air-to-air missile featuring an imaging infrared seeker and a 11 kg blast-fragmentation warhead.

DETAILS: Developed by Israel’s Rafael Advanced Defense Systems, the Python 5 entered service in the early 2000s as a successor to the Python 4. It incorporates a dual-band imaging infrared (IIR) seeker, full-sphere (360°) engagement capability, and lock-on after launch (LOAL) functionality.
These features allow the missile to engage highly maneuverable or even low-signature targets at short and medium ranges. Its thrust-vectoring control and aerodynamic design give it extreme agility, enabling high-G maneuvers in dogfights or when fired off-boresight. The missile is fully compatible with helmet-mounted sights and modern fire control systems, and it can engage targets in cluttered or high-countermeasure environments.

SPECIFICATIONS:
Length: 3 m
Diameter: 160 mm
Wingspan: 0.64 m / 640 mm
Weight: 105 kg
Warhead: 11 kg high-explosive blast-fragmentation
Guidance: Imaging infrared (dual-band IIR), LOAL & LOBL
Speed: ~ Mach 2
Range: 25+ km
Ceiling: >16 km

NOTES:
Initial Operational Capability (IOC): 2003
Platforms: F-15, F-16, F-35, LCA Tejas, JAS 39 Gripen, Kfir, and others
Operators: Israel, India, Brazil, Chile, Colombia, Peru, Singapore, South Africa, Vietnam

SOURCES:
Rafael Advanced Defense Systems: https://www.rafael.co.il/system/python5/
Airforce Technology: https://www.airforce-technology.com/pro ... el-israel/
Army Technology: https://www.army-technology.com/projects/spyder/
Wikipedia: https://en.wikipedia.org/wiki/Python_(missile)
The Aviationist: https://theaviationist.com/2025/01/27/r ... irst-time/

----- Python 5 SPYDER-MR|| Weapon_3167 ----------

OVERVIEW: The Python 5 (surface-launched) is an infrared-guided, beyond-visual-range surface-to-air missile used in the SPYDER-MR system, equipped with a 11 kg blast-fragmentation warhead and capable of engaging targets up to ~20 km away.

DETAILS: In the SPYDER-MR configuration, the Python-5 missile is vertically launched from canisters and fitted with a booster to achieve extended range and faster time-to-target. It uses a dual-band imaging infrared seeker that provides lock-on-before-launch (LOBL) and lock-on-after-launch (LOAL) capability, allowing the missile to engage highly maneuverable targets, even in cluttered or electronically contested environments.
It is capable of intercepting aircraft, UAVs, cruise missiles, and precision-guided munitions. The Python-5's electro-optical guidance ensures high immunity to jamming and flares, making it highly effective for point and area air defense roles.

SPECIFICATIONS:
Missile Type: Python 5 (surface-launched, booster-equipped)
Guidance: Dual-band IIR seeker, LOBL/LOAL capable
Warhead: 11 kg blast-fragmentation, laser proximity and impact fuzed
Range: ~20 km
Ceiling: Up to ~16,000 m
Speed: ~ Mach 2
Radar Integration: EL/M-2084 3D AESA radar
Engagement Capability: Multiple simultaneous targets (up to 60 system-wide, dependent on radar)

NOTES:
Initial Operational Capability (IOC): 2008
Operators: India, Vietnam, Singapore, Georgia, Peru, Philippines, Azerbaijan, Rwanda

SOURCES:
Rafael: https://www.rafael.co.il/worlds/air-def ... er-family/
IAI ELTA: https://www.iai.co.il/p/el-m-2084
Missile Defense Advocacy Alliance: https://missiledefenseadvocacy.org/miss ... ms/spyder/
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
[Jane’s Land-Based Air Defence – SPYDER-MR (subscription)]
Defense Update: https://defense-update.com/spyder-mr-mi ... nse-system

----- Python 5 SPYDER SR|| Weapon_3166 ----------

OVERVIEW: The Python 5 (surface-launched) is a short-range, infrared-guided surface-to-air missile used in the SPYDER-SR system, featuring a 11 kg blast-fragmentation warhead and capable of engaging targets up to ~10 km away.

DETAILS: In the SPYDER-SR system, the Python 5 is launched from a truck-mounted canister without a booster, providing fast-reaction point defense against low-flying and maneuvering threats. It uses a dual-band imaging infrared seeker that enables both Lock-On-Before-Launch (LOBL) and Lock-On-After-Launch (LOAL) modes.
This allows the missile to engage targets with high agility and resistance to countermeasures, including flares and ECM. The SPYDER-SR system integrates an electro-optical surveillance system, the EL/M-2106 radar, and a mobile command-and-control unit to track and engage multiple aerial threats simultaneously. The Python-5’s wide look angle, high maneuverability, and rapid reaction capability make it ideal for defending fixed assets or mobile formations.

SPECIFICATIONS:
Missile Type: Python 5 (surface-launched, without booster)
Guidance: Dual-band IIR seeker, LOBL/LOAL capable
Warhead: 11 kg blast-fragmentation, laser proximity and impact fuzed
Range: ~10 km
Ceiling: Up to ~9,000 m
Speed: ~ Mach 2
Radar Integration: EL/M-2106 ATAR or similar 3D radar
Engagement Capability: Multiple simultaneous targets (dependent on radar and control unit)

NOTES:
Initial Operational Capability (IOC): 2005
Operators: India, Singapore, Georgia, Vietnam, Peru, Philippines, Azerbaijan

SOURCES:
Rafael: https://www.rafael.co.il/worlds/air-def ... er-family/
IAI ELTA: https://www.iai.co.il/p/elm-2106atar
Missile Defense Advocacy Alliance: https://missiledefenseadvocacy.org/miss ... ms/spyder/
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Defense Update: https://defense-update.com/spyder-sr-sh ... nse-system
Jane’s Land-Based Air Defence: SPYDER-SR

Rams128 · Post by **Rams128** » Sun Jun 01, 2025 3:28 pm

SPICE Bombs

----- SPICE 1000 GPS/EO [MK83] || Weapon_278 ----------

OVERVIEW: The SPICE 1000 is an Israeli precision-guided munition developed by Rafael, based on the Mk 83 (454 kg) general-purpose bomb, integrating an electro-optical (EO)/infrared (IR) and GPS/INS guidance kit for stand-off attack with pinpoint accuracy in all weather and GPS-denied environments.

DETAILS: SPICE (Smart, Precise Impact and Cost-Effective) 1000 is a modular guidance kit that converts standard Mk 83-class unguided bombs into precision strike weapons with extended stand-off capability. It combines satellite-aided inertial navigation (GPS/INS) with autonomous electro-optical scene-matching technology for terminal homing, enabling it to strike fixed and relocatable targets without requiring real-time target illumination.

The kit includes mid-body wings for extended range and pop-out tail fins for maneuverability. SPICE 1000 can engage targets at distances of up to 100 km when released from high altitude and speed. The EO-seeker can be loaded with a reference image of the target, making the system jam-resistant and ideal for complex or GPS-contested environments.

SPICE 1000 offers high circular error probable (CEP) accuracy—less than 3 meters—and can operate in day/night and all-weather conditions. It is also capable of automatic target acquisition, target reattack, and “man-in-the-loop” capabilities with real-time video feed for dynamic targeting.

SPECIFICATIONS:
Guidance: Dual-mode: GPS/INS mid-course + EO/IIR terminal homing (scene-matching or man-in-the-loop)
Warhead: Mk 83 (454 kg) general-purpose HE warhead
Range: Up to 100 km (stand-off range)
Accuracy: ≤ 3 m CEP
Length: ~3.0 m (wings folded)
Wingspan: ~1.7 m (deployed)
Weight: ~1,100 kg (with Mk 83 warhead)
Platforms: F-15, F-16, F/A-18, Eurofighter Typhoon, Gripen, Tejas Mk1A, Mirage 2000 (with integration), Rafale (under evaluation)

NOTES:
Initial Operational Capability (IOC): Circa 2005
Operators: Israel, India, Greece, Singapore, Poland, Philippines, Azerbaijan
Combat Use: Believed to have been used by the Israeli Air Force in precision strikes in Syria and Gaza.
Interesting Fact: Unlike laser-guided bombs, SPICE 1000 can engage hidden or camouflaged targets using pre-loaded imagery, allowing it to function independently of GPS or laser designation—a key advantage in modern electronic warfare environments.

SOURCES:
Rafael Advanced Defense Systems - SPICE 1000/2000 Family: https://www.rafael.co.il/system/spice-family-1000-2000/
SPICE 1000 & SPICE 2000 Brochure (PDF): https://www.rafael.co.il/wp-content/upl ... e-2000.pdf
Airforce Technology - IAF's Spice 1000 Munition Attains IOC: https://www.airforce-technology.com/new ... -aircraft/
Wikipedia - SPICE (Bomb): https://en.wikipedia.org/wiki/Spice_(bomb)

----- SPICE 2000 GPS/EO [MK84] || Weapon_461 ----------

OVERVIEW: The SPICE 2000 is a standoff precision-guided munition developed by Rafael Advanced Defense Systems, combining a Mk 84 (907 kg) general-purpose warhead with an advanced dual-mode GPS/EO guidance kit, enabling all-weather, day/night deep-strike capability with exceptional accuracy and resistance to jamming.

DETAILS: SPICE (Smart, Precise Impact, Cost-Effective) 2000 is the largest and most powerful member of the SPICE family, designed to convert standard Mk 84 bombs into precision-guided munitions. It uses a hybrid guidance system combining GPS-aided INS navigation for midcourse flight and electro-optical/IIR terminal guidance via autonomous scene-matching or man-in-the-loop modes.

It features large deployable wings and control surfaces, allowing for stand-off range up to 60–100 km when released at high altitude. Its onboard image processing enables it to engage pre-loaded targets in GPS-denied environments or select targets in real time using live video feed.

SPICE 2000 has a circular error probable (CEP) of <3 meters, making it ideal for strategic strikes on fortified or high-value targets. It has been combat-tested and is actively deployed by multiple air forces, especially in operations requiring minimal collateral damage.

SPECIFICATIONS:
Guidance: Dual-mode — INS/GPS midcourse guidance + EO/IIR terminal seeker with scene-matching and man-in-the-loop capability
Warhead: 907 kg Mk 84 high-explosive general-purpose bomb
Range: 60–100 km (depending on release conditions)
Accuracy: ≤ 3 m CEP
Length: ~4.6 m
Wingspan: ~2.0 m (deployed)
Weight: ~1,130–1,400 kg (varies by configuration)
Compatible Platforms: F-15, F-16, Rafale, Mirage 2000, Tejas Mk1A, Sukhoi Su-30MKI (India), others (with integration)

NOTES:
Initial Operational Capability (IOC): 2003
Operators: Israel, India, Greece, Azerbaijan
Combat Use: Used extensively by the Israeli Air Force in precision strikes in Syria and Gaza; used by India during the 2019 Balakot airstrikes.
Interesting Fact: Unlike JDAMs or laser-guided bombs, SPICE 2000’s autonomous EO guidance allows high-precision engagement in environments with heavy GPS jamming or cloud cover, and enables target discrimination without external illumination.

SOURCES:
Rafael Advanced Defense Systems (Official): https://www.rafael.co.il/system/spice-family-1000-2000/
SPICE 1000/2000 Brochure (PDF): https://www.rafael.co.il/wp-content/upl ... e-2000.pdf
Airforce Technology – SPICE PGMs: https://www.airforce-technology.com/projects/spice/
The Diplomat – India Balakot Strike with SPICE 2000: https://thediplomat.com/2019/03/what-do ... ot-strike/
Janes Air-Launched Weapons (2023 Edition) - SPICE Family Overview

----- SPICE 250 GPS/EO || Weapon_3521 ----------

OVERVIEW: The SPICE 250 is a lightweight, stand-off, air-to-surface guided munition with a 75 kg-class warhead and dual GPS/EO guidance, capable of striking targets up to 100 km away with high precision. It enables high-load carriage and autonomous targeting for modern multirole aircraft.

DETAILS: The SPICE 250 is a fully integrated weapon (not a guidance kit) with fold-out wings and cruciform tail fins, ensuring maneuverability and extended range. It uses GPS/INS for mid-course guidance and EO/IR scene-matching with ATA/ATR for terminal homing, achieving CEP <3 meters. A two-way datalink allows in-flight target updates and mission aborts. Multiple SPICE 250s can be deployed via Smart Quad Rack (SQR), enabling 16 on an F-16 or 28 on an F-15. The ER variant adds a micro turbojet engine, pushing range beyond 150 km.

SPECIFICATIONS:
Guidance: GPS/INS + EO/IR with scene-matching, ATA & ATR
Warhead: ~75 kg blast-fragmentation or penetration
Range: Up to 100 km (SPICE 250); 150+ km (SPICE 250 ER)
Accuracy: ≤ 3 meters CEP
Length: ~1.8 m
Wingspan: ~1.15 m
Weight: ~113 kg
Platforms: F-15, F-16, Mirage 2000, Gripen, FA-50, Tejas Mk1A, others

NOTES:
IOC: 2015 ?
Operators: Israel, Greece, India, Singapore, Poland, Philippines, Brazil
Combat Use: Confirmed use by Israel in operational strikes (details classified)
Interesting Fact: Its compact size and autonomy allow for dense salvo delivery with minimal collateral damage

SOURCES:
Rafael: https://www.rafael.co.il/system/spice-250/
Rafael Brochure (PDF): spice-250-air-to-surface-missile.pdf
Airforce Technology: https://www.airforce-technology.com/pro ... -munition/
Janes (ER variant): https://www.janes.com/osint-insights/de ... evelopment

___________________________________________________

Rams128 · Post by **Rams128** » Sun Jun 01, 2025 9:41 pm

KAB Bombs

----- KAB-1500Kr TV/EO || Weapon_641 ----------

OVERVIEW: The KAB-1500Kr is a Russian 1,500 kg-class air-to-surface guided bomb equipped with a TV-guided seeker, designed for high-precision strikes against hardened or stationary targets in clear weather conditions.

DETAILS: Developed by GNPP Region, the KAB-1500Kr is part of the KAB (Korregiruemaya Aviatsionnaya Bomba) family and is equipped with a television-based electro-optical (EO) seeker. It is manually guided via real-time feed from the seeker, requiring a direct line of sight from the launch aircraft to the target.

The bomb uses mid-body cruciform control fins and large rear stabilizers for flight control and stability. With a powerful 1,500 kg high-explosive or penetration warhead (variants include concrete-piercing Kr-Pr), the KAB-1500Kr is suitable for neutralizing bunkers, fortified positions, and key infrastructure. The TV guidance provides sub-7-meter accuracy under optimal conditions.

SPECIFICATIONS:
Guidance: Electro-optical (TV) terminal homing
Warhead: ~ 675–750 kg high-explosive
Range: ~10–15 km (release altitude dependent)
Accuracy: ≤ 7 meters CEP
Length: ~4.63 m
Wingspan: ~0.85 m
Weight: ~1,500–1,525 kg
Platforms: Su-24M, Su-30MKI, Su-34, Su-35, MiG-29SMT, others

NOTES:
IOC: ~1996
Operators: Russia, India, Algeria, Syria
Combat Use: Used by Russia in Syria against fortified targets; reportedly used by India in trials and certified for Su-30MKI
Interesting Fact: The KAB-1500Kr requires the launch aircraft to maintain line-of-sight during terminal guidance, limiting its use in poor weather or heavily defended airspace

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
GNPP Region / Tactical Missiles Corp.: http://www.ktrv.ru
Rosoboronexport KAB datasheet (archived)
Janes Air-Launched Weapons (latest editions): https://www.janes.com
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Airforce Technology: https://www.airforce-technology.com/dat ... ided-bomb/
Indian Air Force Su-30MKI integration trials reports (open-source)

----- KAB-1500Kr-Pr TV/EO || Weapon_3077 ----------

OVERVIEW: The KAB-1500Kr-Pr is a 1,500 kg-class Russian precision-guided bomb featuring a TV-guided electro-optical seeker and a penetrating warhead, designed for striking hardened underground or reinforced concrete targets.

DETAILS: Developed by GNPP Region as a sub-variant of the KAB-1500Kr family, the Kr-Pr version (where "Pr" stands for penetrator) is equipped with a reinforced, concrete-piercing warhead and a TV-guided seeker that allows precise terminal homing. The munition is guided in real-time by the launch aircraft via a TV feed, requiring continuous line-of-sight during the terminal phase.

Optimized for destruction of underground bunkers, command centers, and reinforced structures, the KAB-1500Kr-Pr delivers deep penetration before detonation, ensuring destruction of protected targets. Like other Kr-series bombs, it uses cruciform control fins and is released from medium or high altitude.

SPECIFICATIONS:
Guidance: Electro-optical (TV) terminal homing
Warhead: ~ 675–750 kg penetration warhead
Range: ~10–15 km (altitude dependent)
Accuracy: ≤ 7 meters CEP
Length: ~4.63 m
Wingspan: ~0.85 m
Weight: ~1,525 kg
Platforms: Su-24M, Su-30MKI, Su-34, Su-35, MiG-29SMT, others

NOTES;
IOC: ~1996
Operators: Russia, India, Algeria
Combat Use: Believed to have been used by Russia in Syria against deeply buried facilities and bunkers
Interesting Fact: The KAB-1500Kr-Pr's penetrator warhead enables it to breach several meters of reinforced concrete before detonation, making it one of the most powerful bunker-busting bombs in Russian inventory

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
GNPP Region / Tactical Missiles Corporation: http://www.ktrv.ru
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Janes Air-Launched Weapons (latest editions): https://www.janes.com
Airforce Technology Profile: https://www.airforce-technology.com/dat ... ided-bomb/
Rosoboronexport Product Catalogs (archived PDFs)

----- KAB-1500L-F LGB || Weapon_639 ----------

OVERVIEW: The KAB-1500L-F is a 1,500 kg-class Russian laser-guided air-to-surface bomb equipped with a high-explosive blast-fragmentation warhead, intended for precision strikes against fortified ground targets and enemy infrastructure.

DETAILS: Designed by GNPP Region, the KAB-1500L-F is part of Russia’s KAB-1500L series of precision-guided munitions. The “L” denotes semi-active laser guidance, while “F” refers to a high-explosive fragmentation warhead. The bomb is guided by a semi-active laser seeker that homes in on reflected laser energy from a designated target, either by the launching aircraft or an external designator.

Intended for destroying large, soft or semi-hardened area targets—such as industrial facilities, ammo depots, and airfield infrastructure, the KAB-1500L-F offers improved accuracy over conventional bombs, especially from medium to high altitudes. The weapon is compatible with a variety of Russian multirole combat aircraft and maintains high terminal accuracy, making it a reliable option for strategic precision bombing.

SPECIFICATIONS:
Guidance: Semi-active laser homing
Warhead: ~ 675–750 kg high-explosive blast-fragmentation
Range: ~10–15 km (altitude dependent)
Accuracy: ≤ 7 meters CEP
Length: ~4.63 m
Wingspan: ~0.85 m
Weight: ~1,525 kg
Platforms: Su-24M, Su-30MKI, Su-34, Su-35, MiG-29SMT, others

NOTES:
IOC: 1995
Operators: Russia, India, Algeria, Syria
Combat Use: Confirmed use in Syria by Russian aircraft against fixed infrastructure and fortified positions
Interesting Fact: While similar in design to U.S. Paveway-series LGBs, the KAB-1500L-F carries nearly double the warhead mass of a GBU-16, providing a much larger blast effect

SOURCES:
https://www.deagel.com/Weapons/KAB/a001035
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
GNPP Region / KTRV: http://www.ktrv.ru
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Janes Air-Launched Weapons (latest editions): https://www.janes.com
Airforce Technology KAB Series Overview: https://www.airforce-technology.com/dat ... ded-bombs/
Russian Ministry of Defence Reports & Briefings (archived releases)

----- KAB-1500L-Pr LGB || Weapon_49 ----------

OVERVIEW: The KAB-1500L-Pr is a 1 500 kg-class Russian laser-guided air-to-surface bomb fitted with a deep-penetration warhead for destroying hardened underground or reinforced-concrete targets with high precision.

DETAILS: Designed by GNPP Region (Tactical Missiles Corporation), the bomb belongs to the KAB-1500L family: “L” denotes semi-active laser guidance, “Pr” (penetrator) identifies the reinforced casing and delayed-action fuze. A semi-active laser seeker homes on reflected laser energy from either the launch aircraft or an external designator, giving a CEP of < 7 m from medium- or high-altitude release. The weapon is routinely carried by frontline Russian strike fighters such as the Su-24M and Su-34. Its penetrator warhead can breach several metres of reinforced concrete before detonation, making it suitable for bunkers, C2 nodes and aircraft shelters.

SPECIFICATIONS:
Guidance:Semi-active laser homing
Warhead: ~675–750 kg penetrating HE (delayed-action fuze)
Range: ~10–15 km (release-altitude dependent)
Accuracy: ≤ 7 m CEP
Length: ~4.63 m
Wingspan: ~0.85 m
Weight: ~1 525 kg
Platforms: Su-24M, Su-30MKI/SM, Su-34, Su-35S, MiG-29SMT

NOTES:
IOC: 1987 first operational deliveries to Soviet Frontal Aviation; penetrator variant reached units alongside baseline KAB-1500L.
Operators: Russia, India, Algeria (limited stocks), Syria (supplied via Russia).
Combat Use: Reported Russian employment in Syria (2015-present) against deeply buried command bunkers near Hama and Palmyra.
Interesting Fact: Russian test data credit the KAB-1500L-Pr with penetration of ≈ 3 m of reinforced concrete or ≈ 20 m of earth before detonation.

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
Tactical Missiles Corporation / GNPP Region product overview: https://ktrv.ru
Jane’s Air-Launched Weapons (latest editions KAB-1500L series entry): https://www.janes.com
SIPRI Arms Transfers Database KAB-1500 exports: https://armstrade.sipri.org
Airforce Technology KAB series profile: https://www.airforce-technology.com/dat ... ded-bombs/
MilitaryRussia.ru KAB-1500L family specifications (archived): http://militaryrussia.ru/blog/topic-595.html
AusAirPower Russian Guided Bombs technical survey: https://www.ausairpower.net/APA-Rus-GBU.html

----- KAB-250LG-E || Weapon_3578 ----------

OVERVIEW: The KAB-250LG-E is a lightweight, precision-guided, air-to-surface bomb developed by Russia, using semi-active laser guidance and designed for high-accuracy strikes against small, high-value ground targets with minimal collateral damage.

DETAILS: Developed by GNPP Region, the KAB-250LG-E is an export-oriented, 250 kg-class guided bomb utilizing a semi-active laser seeker. It is compatible with a wide range of modern Russian combat aircraft such as the Su-30SM, Su-34, Su-35, and MiG-35. The weapon's aerodynamic shape and guidance system allow precision strikes with a CEP of ≤ 5 meters, making it suitable for use in urban or constrained environments where reduced blast radius and target discrimination are essential.

It follows the general design philosophy of Russian KAB-series bombs, offering a balance between size, accuracy, and cost-efficiency. The smaller warhead size makes it comparable in concept to Western Paveway II-type munitions (e.g., GBU-12).

SPECIFICATIONS:
Guidance: Semi-active laser homing
Warhead: ~100 kg HE fragmentation
Range: ~10–17 km (altitude dependent)
Accuracy: ≤ 5 meters CEP
Length: ~3.2 m
Diameter: ~255 mm
Wingspan: ~0.55 m
Weight: ~256–265 kg
Platforms: Su-30SM, Su-34, Su-35S, MiG-29SMT, MiG-35, Yak-130 (with modifications)

NOTES:
IOC: 2019 (export version announced at MAKS 2019; trials and initial service entry with RuAF units likely in late 2010s).
Operators: Russia, Algeria (reported), and potential clients in Southeast Asia and MENA
Interesting Fact: The KAB-250LG-E is designed to be compatible with Russia’s fifth-generation aircraft like the Su-57, owing to its compact form factor and internal bay compatibility.

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
Tactical Missiles Corporation (KTRV): http://www.ktrv.ru
MAKS 2019 Official Displays and Product Sheets
Jane’s Air-Launched Weapons – KAB-250LG-E profile: https://www.janes.com
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Airforce Technology – KAB-series overview: https://www.airforce-technology.com/dat ... ded-bombs/
MilitaryRussia.ru: http://militaryrussia.ru/blog/topic-595.html
AusAirPower – Russian precision-guided munitions overview: https://www.ausairpower.net/APA-Rus-GBU.html

----- KAB-250S-E GLONASS || Weapon_3579 ----------

OVERVIEW: The KAB-250S-E is a 250 kg-class Russian satellite-guided glide bomb that uses GLONASS-aided inertial navigation to deliver a ~120 kg high-explosive warhead with ≤ 10 m CEP at stand-off ranges of up to 40 km.

DETAILS: Developed by GNPP Region / Tactical Missiles Corporation, the KAB-250S-E (“S” = satellite guidance, “E” = export) is the all-weather counterpart to the laser-guided KAB-250LG-E. The bomb employs an INS unit updated in flight by Russia’s GLONASS constellation; once released it glides on pop-out wings and cruciform tail fins to the programmed impact point, requiring no target illumination. It was first shown at MAKS-2015 and cleared for export after state trials with RuAF Su-34s and Su-35S fighters. Compact dimensions let four KAB-250S-E fit on a standard twin-rail launcher or inside the weapons bay of the Su-57.

SPECIFICATIONS:
Parameter: Value
Guidance: GLONASS-aided INS (fire-and-forget)
Warhead: ~100 kg HE fragmentation
Range: 12 km (low-alt) – 40 km (high-alt glide)
Accuracy: ≤ 10 m CEP (typ. 3–7 m under optimal geometry)
Length: ~3.2 m
Diameter: 255 mm
Wingspan: ~0.55 m (deployed)
Total Weight: 250 – 265 kg
Platforms: Su-30SM, Su-34, Su-35S, MiG-35, Su-57; export integration offered for Su-30/35, MiG-29/35

NOTES:
IOC: 2020 (entered limited service with Russian Aerospace Forces after flight-test series 2017-2019).
Operators: Russia (in service), Algeria and India have shown interest but no publicly confirmed deliveries as of 2025.
Interesting Fact: Because it relies solely on satellite/INS guidance, KAB-250S-E can attack through cloud cover and dust storms—conditions that impede the laser-guided KAB-250LG-E.

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
Tactical Missiles Corp. (KTRV) product sheet (MAKS-2021): https://ktrv.ru
TASS “Russia completes trials of KAB-250S-E precision bomb” (Dec 2020): https://tass.com/defense/1241311
Jane’s Air-Launched Weapons - KAB-250S-E entry: https://www.janes.com
Airforce Technology Russian - KAB-250 family overview: https://www.airforce-technology.com/dat ... ded-bombs/
SIPRI Arms Transfers Database - search “KAB-250” exports: https://armstrade.sipri.org

----- KAB-500L LGB || Weapon_1035 ----------

OVERVIEW: The KAB-500L is a 500 kg-class Russian precision-guided bomb with a semi-active laser seeker, designed for use against stationary, high-value targets. It features a high-explosive fragmentation warhead and offers significant accuracy improvements over unguided munitions.

DETAILS: Developed by GNPP Region, the KAB-500L is Russia’s standard laser-guided bomb and has been in operational use since the late 1980s. The bomb consists of a standard FAB-500M-62 body fitted with a laser seeker and guidance module. It uses reflected laser energy from a designator (airborne or ground-based) to home in on the target. Upon release, the bomb deploys control fins to steer toward the illuminated point, with accuracy typically within 5–7 meters CEP.

The KAB-500L has been widely integrated on Russian and export fighter-bomber platforms and is often seen as a functional analogue to the U.S. GBU-12 Paveway II, albeit with a larger warhead. It’s designed to destroy bunkers, runways, infrastructure, and fixed high-value assets.

SPECIFICATIONS:
Guidance: Semi-active laser homing
Warhead: ~210 kg high-explosive fragmentation (from FAB-500M-62)
Range: ~10–15 km (release altitude dependent)
Accuracy: ≤ 7 meters CEP
Length: ~3.05 m
Diameter: ~0.4 m
Wingspan: ~0.75 m
Total Weight: ~525 kg
Platforms: Su-24M, Su-30SM, Su-34, Su-35, MiG-29SMT, MiG-35, others

NOTES:
IOC: 1979
Operators: Russia, India, Algeria, Syria, Angola, Vietnam
Combat Use: Used by Russian forces in Chechnya, Syria, and Ukraine for precision strikes
Interesting Fact: The KAB-500L is based on a conventional iron bomb, but achieves PGM-level accuracy using Soviet-era laser guidance—a cost-effective upgrade path later mirrored by several other countries.

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
KTRV / GNPP Region official site: http://www.ktrv.ru
Airforce Technology - KAB Series Overview: https://www.airforce-technology.com/dat ... ded-bombs/
Jane’s Air-Launched Weapons (Latest editions): https://www.janes.com
SIPRI Arms Transfers Database: https://armstrade.sipri.org
TASS News Agency (archival reporting): https://tass.com/defense
Russian MoD and RuAF press footage confirming KAB-500L use in Syria (2015–2017)

----- KAB-500S GLONASS || Weapon_3340 ----------

OVERVIEW: The KAB-500S-E is a 500 kg-class Russian satellite-guided precision bomb utilizing GLONASS-aided inertial navigation. It is designed for high-accuracy strikes against stationary ground targets under all weather conditions and is considered Russia’s analogue to the U.S. JDAM series.

DETAILS: Developed by GNPP Region (a division of Tactical Missiles Corporation), the KAB-500S-E is Russia’s first operational satellite-guided bomb. It is based on the standard FAB-500 general-purpose bomb body, fitted with a GLONASS-aided inertial navigation system and a tail guidance module with control fins. This configuration allows for high-precision targeting without the need for external laser designation.

The KAB-500S-E is intended for use against a variety of fixed targets, including command centers, infrastructure, and fortified facilities. It has been integrated into various Russian aircraft platforms, such as the Su-24M, Su-30SM, Su-34, Su-35S, and MiG-35. The bomb has seen combat use in Syria and Ukraine.

SPECIFICATIONS:
Guidance: GLONASS-aided inertial navigation
Warhead: ~210 kg high-explosive blast-fragmentation
Range: ~40 km (release altitude dependent)
Accuracy: ≤ 10 meters CEP
Length: ~3.1 m
Diameter: ~0.4 m
Wingspan: ~0.75 m
Total Weight: ~560 kg
Platforms: Su-24M, Su-30SM, Su-34, Su-35S, MiG-35, others

NOTES:
IOC: 2007 (entered service with the Russian Aerospace Forces)
Operators: Russia
Combat Use: Employed by Russian forces in Syria and Ukraine for precision strikes
Interesting Fact: The KAB-500S-E represents Russia's move towards satellite-guided munitions, providing all-weather, day-night operational capability without reliance on external target illumination.

SOURCES:
Ausairpower: https://www.ausairpower.net/APA-Rus-GBU.html
Rosoboronexport Product Page (Archived): https://roe.ru/eng/catalog/aerospace-sy ... ab-500s-e/
Airforce Technology KAB Series Overview: https://www.airforce-technology.com/dat ... ded-bombs/
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Jane’s Air-Launched Weapons (latest editions): https://www.janes.com
KTRV Official Website: http://www.ktrv.ru

CV60 · Post by **CV60** » Mon Jun 02, 2025 6:47 pm

Rams-Tank you very much for these. I'll get them in the next update!

Rams128 · Post by **Rams128** » Tue Jun 03, 2025 6:18 pm

AIM/MIM/RIM-7 SPARROW Missiles

----- AIM-7E Sparrow III || Weapon_181 ----------

OVERVIEW: The AIM-7E Sparrow III is a U.S. semi-active radar-guided air-to-air missile developed in the early 1960s for medium-range engagements. Widely used during the Vietnam War, it became the backbone of Western BVR (Beyond Visual Range) air combat.

DETAILS: An improved version of earlier Sparrow models, the AIM-7E featured solid-state electronics, a more reliable seeker, and a blast-fragmentation warhead. It relied on continuous radar illumination from the launch platform and underwent multiple subvariant upgrades (e.g., AIM-7E-2, AIM-7E-3) to address maneuverability and ECM resilience. Despite early reliability issues in Vietnam, it became a standard loadout for the F-4 Phantom II and later adapted to aircraft like the F-14 and F-15.

SPECIFICATIONS:
Guidance: Semi-active radar homing
Warhead: 30.5 kg high-explosive blast-fragmentation
Accuracy: Dependent on radar lock; limited in look-down/shoot-down
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 0.81 m
Total Weight: 230 kg
Platforms: F-4 Phantom II, F-14 Tomcat, F-15 Eagle, F-16 Fighting Falcon (early blocks), F-104S

Range: 35 km (variant and altitude dependent)
Speed: Mach 4+
Maneuverability: Up to 10 G Rear control fins, roll-stabilized, limited close-in agility

NOTES:
IOC: 1963 (U.S. Navy service as AIM-N-6b, later redesignated AIM-7E)
Operators: United States, United Kingdom, Canada, Australia, Japan, Italy, Germany, Greece, Turkey, Israel, Saudi Arabia, Iran (pre-1979), South Korea, Taiwan, Spain, Egypt, Thailand, Pakistan, Jordan
Combat Use: Deployed extensively during the Vietnam War (approx. 612 launched), Middle East conflicts (1973, 1982), and Gulf War
Interesting Fact: The AIM-7E’s Vietnam-era performance led to critical evaluations of missile doctrine and later advances in air combat tactics and missile reliability.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
U.S. Navy Fact File (Archived): https://www.navy.mil/Resources/Fact-Files/
Raytheon Missiles & Defense: https://www.raytheonmissilesanddefense.com
Jane’s Air-Launched Weapons: https://www.janes.com
National Museum of the U.S. Air Force: https://www.nationalmuseum.af.mil/
“Clashes: Air Combat over North Vietnam” by Michel III, Marshall L.
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
https://en.wikipedia.org/wiki/AIM-7_Sparrow

----- AIM-7E4 Sparrow III || Weapon_431 ----------

OVERVIEW: The AIM-7E-4 Sparrow III is a medium-range, semi-active radar-guided air-to-air missile designed for beyond-visual-range engagements, featuring improved reliability, electronic counter-countermeasures (ECCM), and enhanced performance over earlier Sparrow E variants.

DETAILS: The AIM-7E-4 was developed as a response to performance issues observed in earlier AIM-7E variants, particularly against maneuvering or ECM-equipped targets. It featured enhanced guidance electronics and better resistance to electronic jamming, increasing kill probability in combat. Though retaining the same airframe and propulsion as its predecessors, internal modifications made it more reliable and effective in BVR engagements. It remained in service until gradually replaced by the AIM-7F in the late 1970s.

SPECIFICATIONS:
Guidance: Semi-active radar homing
Warhead: 30.5 kg high-explosive blast-fragmentation
Accuracy: Improved ECCM; still dependent on radar lock
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 0.81 m
Total Weight: 230 kg
Platforms: F-4 Phantom II, F-14 Tomcat, F-15 Eagle, F-104S

Range: 35 km (altitude and launch conditions dependent)
Speed: Mach 4+
Maneuverability: up to 18–20 g during terminal phase (limited against high-G targets)

NOTES:
IOC: 1973 (entered service as the final AIM-7E model)
Operators: United States, United Kingdom, Canada, Australia, Japan, Italy, Germany, Greece, Turkey, Israel, Saudi Arabia, Iran (pre-1979), South Korea, Taiwan, Spain, Egypt, Thailand, Pakistan, Jordan
Combat Use: Used in late Vietnam War air engagements, including Operation Linebacker I & II; also exported to NATO and allied air forces
Interesting Fact: The AIM-7E-4 addressed many of the failings of earlier Sparrow versions in Vietnam, achieving significantly better performance and forming the bridge to the digital AIM-7F.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
U.S. Navy Fact File (Archived): https://www.navy.mil/Resources/Fact-Files/
Raytheon Missiles & Defense: https://www.raytheonmissilesanddefense.com
Jane’s Air-Launched Weapons: https://www.janes.com
National Museum of the U.S. Air Force: https://www.nationalmuseum.af.mil/
“Clashes: Air Combat over North Vietnam” by Michel III, Marshall L.
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
https://en.wikipedia.org/wiki/AIM-7_Sparrow

----- AIM-7F Sparrow III || Weapon_150 ----------

OVERVIEW: The AIM-7F Sparrow III is a medium-to-long range, semi-active radar-guided air-to-air missile developed by the United States, featuring major improvements in range, electronics, and reliability over previous Sparrow variants.

DETAILS: Introduced in the mid-1970s, the AIM-7F incorporated a solid-state guidance system, improved monopulse seeker, and a dual-stage solid rocket motor that significantly extended its range. It also featured a new modular design separating the warhead and guidance sections, which simplified upgrades and maintenance. The AIM-7F was compatible with pulse-Doppler radar systems and was fully integrated with modern fighters like the F-15 and F-14, offering greatly enhanced BVR capability. It remained in widespread service through the 1980s and was exported extensively.

SPECIFICATIONS:
Guidance: Semi-active radar homing (monopulse seeker)
Warhead: 39 kg continuous-rod high-explosive
Accuracy: All-aspect capability with improved target discrimination
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 231 kg
Platforms: F-4 Phantom II, F-14 Tomcat, F-15 Eagle, F-16 Fighting Falcon (Block 15/25), F-104S ASA

Range: 70 km (altitude and launch profile dependent)
Speed: Mach 4+
Maneuverability: Up to 18 g in terminal phase (with improved control response over E variants)

NOTES:
IOC: 1976 (entered USAF service with the F-15A)
Operators: United States, United Kingdom, Canada, Australia, Japan, Italy, Germany, Greece, Turkey, Israel, Saudi Arabia, South Korea, Taiwan, Spain, Egypt, Thailand, Pakistan, Jordan, Iran (pre-1979)
Combat Use: Used in multiple Cold War-era conflicts; widely deployed by F-15s and F-14s during the late 1970s–1990s
Interesting Fact: The AIM-7F marked the transition from analog to digital components in the Sparrow series and introduced significant range and reliability improvements over the AIM-7E.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
U.S. Navy Fact File (Archived): https://www.navy.mil/Resources/Fact-Files/
Raytheon Missiles & Defense: https://www.raytheonmissilesanddefense.com
Jane’s Air-Launched Weapons: https://www.janes.com
National Museum of the U.S. Air Force: https://www.nationalmuseum.af.mil/
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
https://en.wikipedia.org/wiki/AIM-7_Sparrow

----- AIM-7M Sparrow|| Weapon_1400 ----------

OVERVIEW: The AIM-7M Sparrow III is a medium-to-long range, semi-active radar-guided air-to-air missile with digital guidance and improved all-weather, look-down/shoot-down performance, representing the most capable operational Sparrow variant before the AIM-120 AMRAAM.

DETAILS: Introduced in the early 1980s, the AIM-7M featured a new inverse monopulse seeker, a digital programmable signal processor for improved target tracking in cluttered environments, and significantly enhanced electronic counter-countermeasures (ECCM). It retained the AIM-7F’s dual-stage motor and modular design but offered vastly improved reliability, accuracy, and lethality. The missile was widely integrated with aircraft like the F-14, F-15, F-16, and F/A-18. It saw extensive use in the Gulf War, where it achieved a much-improved kill ratio compared to earlier variants.

SPECIFICATIONS:
Guidance: Semi-active radar homing (inverse monopulse seeker with digital processor)
Warhead: 39 kg continuous-rod high-explosive
Accuracy: All-aspect, look-down/shoot-down capable with ECCM
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 231 kg
Platforms: F-14 Tomcat, F-15 Eagle, F-16 Fighting Falcon (Block 25+), F/A-18 Hornet

Range: 70 km (altitude and launch conditions dependent)
Speed: Mach 4+
Maneuverability: Up to 18 g in terminal phase (enhanced tracking and control responsiveness)

NOTES:
IOC: 1982 (entered service with the U.S. Navy and USAF)
Operators: United States, United Kingdom, Canada, Australia, Japan, Italy, Germany, Greece, Turkey, Israel, Saudi Arabia, South Korea, Taiwan, Spain, Egypt, Thailand, Pakistan, Jordan, Iran (pre-1979)
Combat Use: Used with high effectiveness in the 1991 Gulf War; also deployed by multiple NATO and allied air forces in the 1990s
Interesting Fact: The AIM-7M achieved the highest combat effectiveness of all Sparrow variants, credited with 24 air-to-air kills during Operation Desert Storm.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
U.S. Navy Fact File (Archived): https://www.navy.mil/Resources/Fact-Files/
Raytheon Missiles & Defense: https://www.raytheonmissilesanddefense.com
Jane’s Air-Launched Weapons: https://www.janes.com
National Museum of the U.S. Air Force: https://www.nationalmuseum.af.mil/
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
https://en.wikipedia.org/wiki/AIM-7_Sparrow

----- AIM-7P Sparrow || Weapon_443 ----------

OVERVIEW: The AIM-7P Sparrow III is a late-generation, medium-to-long range, semi-active radar-guided air-to-air missile featuring upgraded guidance, enhanced low-altitude performance, and improved ECCM capabilities over the AIM-7M.

DETAILS: Developed in the 1990s, the AIM-7P was an incremental upgrade to the AIM-7M, introducing a reprogrammable digital processor and improved look-down/shoot-down capability, particularly in cluttered environments. It came in two blocks: Block I introduced software-updatable memory, while Block II added GPS interface and midcourse guidance update capability, enhancing lethality against maneuvering targets at longer ranges. Although its combat use was limited, the AIM-7P extended the service life of the Sparrow family until it was largely replaced by the AIM-120 AMRAAM.

SPECIFICATIONS:
Guidance: Semi-active radar homing (inverse monopulse seeker with reprogrammable digital processor)
Warhead: 39 kg continuous-rod high-explosive
Accuracy: High; GPS-aided midcourse update (Block II), improved target discrimination in ground clutter
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 231 kg
Platforms: F-14 Tomcat, F-15 Eagle, F-16 Fighting Falcon (Block 30/32+), F/A-18 Hornet

Range: 70+ km (launch conditions and update capability dependent)
Speed: Mach 4+
Maneuverability: Up to 18 g in terminal phase (retained from AIM-7M, enhanced with better midcourse tracking)

NOTES:
IOC: 1991 (Block I); mid-1990s for Block II
Operators: United States, Japan, Italy, Saudi Arabia, South Korea, Taiwan, Egypt, Turkey (limited export due to AIM-120 replacement)
Combat Use: No confirmed kills; fielded primarily during the transition period to AIM-120
Interesting Fact: The AIM-7P was the only Sparrow variant with optional GPS midcourse updates, bridging analog-era designs with modern digital BVR systems.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
Raytheon Missiles & Defense: https://www.raytheonmissilesanddefense.com
Jane’s Air-Launched Weapons: https://www.janes.com
U.S. Navy Fact File (Archived): https://www.navy.mil/Resources/Fact-Files/
National Museum of the U.S. Air Force: https://www.nationalmuseum.af.mil/
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
https://en.wikipedia.org/wiki/AIM-7_Sparrow

----- MIM-7F SPARROW || Weapon_121 ----------

OVERVIEW: The MIM-7F Sparrow is a U.S. medium-range, semi-active radar-guided surface-to-air missile adapted from the AIM-7F air-to-air missile, designed for ground-based air defense with enhanced range and guidance capabilities.

DETAILS: The MIM-7F is a surface-launched variant of the AIM-7F Sparrow III, integrated into systems like the Skyguard/Sparrow air defense system. It employs a semi-active radar homing guidance system, requiring continuous illumination of the target by ground-based radar. The missile features a dual-thrust solid-propellant rocket motor, providing improved range and speed over earlier versions. Its warhead is a 39 kg continuous-rod high-explosive type, designed to effectively engage high-speed aerial targets. The MIM-7F has been deployed by various countries for point defense against aircraft and missiles.

SPECIFICATIONS:
Guidance: Semi-active radar homing
Warhead: 39 kg continuous-rod high-explosive
Accuracy: Dependent on radar lock; effective in all-weather conditions
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 227–233.6 kg
Platforms: Ground-based launchers (e.g., Skyguard/Sparrow system)

Range: Up to 45 km (variant and altitude dependent)
Speed: Mach 4+
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: 1977
Operators: United States, Greece, Turkey, Egypt, South Korea, Taiwan, Spain, Italy, Germany
Combat Use: Deployed in various air defense roles; specific combat engagements are not widely documented
Interesting Fact: The MIM-7F adapts the air-to-air AIM-7F for surface-to-air applications, extending the versatility of the Sparrow missile family.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
Jane’s Land-Based Air Defence 2002–2003
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

----- MIM-7M Sparrow || Weapon_120 ----------

OVERVIEW: The MIM-7M Sparrow is a U.S. medium-range, semi-active radar-guided surface-to-air missile, adapted from the AIM-7M air-to-air missile, featuring enhanced guidance, improved low-altitude performance, and robust electronic counter-countermeasures (ECCM).

DETAILS: Introduced in the early 1980s, the MIM-7M is a surface-launched variant of the AIM-7M Sparrow III, integrated into ground-based air defense systems such as the Skyguard/Sparrow. It employs an inverse monopulse seeker and a digital programmable signal processor, enhancing target tracking in cluttered environments and improving resistance to electronic countermeasures. The missile utilizes a dual-thrust solid-propellant rocket motor, providing rapid acceleration and sustained flight. Its warhead is a 39 kg continuous-rod high-explosive type, designed to effectively engage high-speed aerial targets. The MIM-7M has been deployed by various countries for point defense against aircraft and missiles.

SPECIFICATIONS:
Guidance: Semi-active radar homing (inverse monopulse seeker with digital processor)
Warhead: 39 kg continuous-rod high-explosive
Accuracy: All-aspect, look-down/shoot-down capable with ECCM
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 231 kg
Platforms: Ground-based launchers (e.g., Skyguard/Sparrow system)

Range: Up to 45 km (launch conditions dependent)
Speed: Mach 4+
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: 1983
Operators: United States, Greece, Egypt, South Korea, Taiwan, Spain, Italy, Germany
Combat Use: Deployed in various air defense roles; specific combat engagements are not widely documented
Interesting Fact: The MIM-7M adapts the air-to-air AIM-7M for surface-to-air applications, extending the versatility of the Sparrow missile family.

SOURCES:
Federation of American Scientists (FAS): https://fas.org/man/dod-101/sys/missile/aim-7.htm
Jane’s Land-Based Air Defence 2002–2003
SIPRI Arms Transfers Database: https://www.sipri.org/databases/armstransfers
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

----- RIM-7E Sea Sparrow || Weapon_1609 ----------

OVERVIEW: The RIM-7E Sea Sparrow is a U.S. ship-launched, short-range, semi-active radar-guided surface-to-air missile, adapted from the AIM-7E Sparrow air-to-air missile. It was the first navalized version, providing point defense against aerial threats.

DETAILS: Introduced in the early 1970s, the RIM-7E was essentially an unmodified AIM-7E adapted for shipboard use. It was launched from the Mk 25 Guided Missile Launching System (GMLS), a modified ASROC launcher . The missile featured fixed wings and was guided by continuous wave radar illumination, requiring manual tracking and engagement. The system provided a rapid solution for enhancing shipboard air defense capabilities against high-speed, low-altitude threats, such as anti-ship missiles and aircraft .

SPECIFICATIONS:
Guidance: Semi-active radar homing
Warhead: 39 kg (86 lbs) blast-fragmentation
Accuracy: Dependent on radar lock; limited in look-down/shoot-down scenarios
Length: 3.66 m (12 ft)
Diameter: 0.203 m (8 in)
Wingspan: 1.02 m (40.2 in)
Total Weight: 230 kg (510 lbs)
Platforms: Mk 25 GMLS (modified ASROC launcher)

Range: Approximately 19 km (10 nmi)
Speed: Mach 4+
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: Early 1970s
Operators: United States, Japan
Combat Use: Deployed for ship self-defense; specific combat engagements are not widely documented
Interesting Fact: The RIM-7E's adaptation marked the beginning of the Sea Sparrow missile family, leading to subsequent enhancements in naval air defense systems.

SOURCES:
U.S. Navy Fact File: https://www.navy.mil/Resources/Fact-Fil ... ile-rim-7/
Weaponsystems.net: https://weaponsystems.net/system/1391-R ... %2BSparrow
U.S. Naval Institute: https://www.usni.org/magazines/naval-hi ... ile-system
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

----- RIM-7H Sea Sparrow || Weapon_1604 ----------

OVERVIEW: The RIM-7H Sea Sparrow is a ship-launched, short-range, semi-active radar-guided surface-to-air missile, adapted from the AIM-7E Sparrow air-to-air missile. It features folding wings for compatibility with the Mk 29 launcher, enhancing naval air defense capabilities.

DETAILS: Introduced in the early 1970s, the RIM-7H is an improved variant of the RIM-7E, designed specifically for shipboard use. The primary enhancement is the incorporation of folding wings and clipped tail fins, allowing the missile to be launched from the compact Mk 29 Guided Missile Launching System (GMLS). This adaptation enabled installation on a wider range of naval vessels. The missile retains the semi-active radar homing guidance system of its predecessor, requiring continuous radar illumination from the ship's fire control system during flight. The RIM-7H provided improved maneuverability and reliability over earlier models, serving as a transitional design leading to more advanced Sea Sparrow variants.

SPECIFICATIONS:
Guidance: Semi-active radar homing
Warhead: 39 kg (86 lbs) blast-fragmentation
Accuracy: Dependent on radar lock; limited in look-down/shoot-down scenarios
Length: 3.66 m (12 ft)
Diameter: 0.203 m (8 in)
Wingspan: 1.02 m (40.2 in)
Total Weight: 230 kg (510 lbs)
Platforms: Mk 29 GMLS

Range: Approximately 19 km (10 nmi)
Speed: Mach 2.5
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: 1973
Operators: United States, NATO member navies
Combat Use: Deployed for ship self-defense; specific combat engagements are not widely documented
Interesting Fact: The RIM-7H's design modifications for shipboard compatibility paved the way for subsequent Sea Sparrow variants with enhanced capabilities.

SOURCES:
U.S. Navy Fact File: https://www.navy.mil/Resources/Fact-Fil ... ile-rim-7/
Weaponsystems.net: https://weaponsystems.net/system/1391-R ... %2BSparrow
Missile Defense Advocacy Alliance: https://missiledefenseadvocacy.org/defe ... a-sparrow/
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

----- RIM-7J Sea Sparrow || Weapon_677 ----------

OVERVIEW: The RIM-7J Sea Sparrow is a U.S. ship-launched, short-range, semi-active radar-guided surface-to-air missile, adapted from the AIM-7F Sparrow air-to-air missile. It incorporates solid-state electronics and a dual-thrust motor, enhancing naval air defense capabilities.

DETAILS: Introduced in the late 1970s, the RIM-7J is a naval variant of the AIM-7F Sparrow III, integrated into the Mk 29 Guided Missile Launching System (GMLS). The missile features a dual-thrust solid-propellant rocket motor, providing improved range and speed over earlier versions. Its warhead is a 39 kg blast-fragmentation type, designed to effectively engage high-speed aerial targets. The RIM-7J employs a semi-active radar homing guidance system, requiring continuous illumination of the target by the ship's radar. This variant offered improved performance against low-altitude threats and served as a transitional design leading to more advanced Sea Sparrow versions.

SPECIFICATIONS:
Guidance: Semi-active radar homing
Warhead: 39 kg blast-fragmentation
Accuracy: Dependent on radar lock; limited in look-down/shoot-down scenarios
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 230 kg
Platforms: Mk 29 GMLS

Range: Approximately 19 km
Speed: Mach 2.5
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: Late 1970s
Operators: United States, NATO member navies
Combat Use: Deployed for ship self-defense; specific combat engagements are not widely documented
Interesting Fact: The RIM-7J's enhancements over previous models improved naval defense against low-flying threats, setting the stage for subsequent Sea Sparrow advancements.

SOURCES:
U.S. Navy Fact File: https://www.navy.mil/Resources/Fact-Fil ... ile-rim-7/
Weaponsystems.net: https://weaponsystems.net/system/1391-R ... %2BSparrow
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

----- RIM-7M Sea Sparrow || Weapon_1687 ----------

OVERVIEW: The RIM-7M Sea Sparrow is a U.S. ship-launched, short-range, semi-active radar-guided surface-to-air missile, adapted from the AIM-7M Sparrow air-to-air missile. It features a monopulse seeker and improved low-altitude performance, enhancing naval air defense capabilities.

DETAILS: Introduced in the early 1980s, the RIM-7M is a naval variant of the AIM-7M Sparrow III, integrated into the Mk 29 Guided Missile Launching System (GMLS). The missile incorporates a monopulse radar seeker and a digital signal processor, providing improved target tracking and resistance to electronic countermeasures. Its warhead is a 39 kg blast-fragmentation type, designed to effectively engage high-speed aerial targets. The RIM-7M employs a semi-active radar homing guidance system, requiring continuous illumination of the target by the ship's radar. This variant offered enhanced performance against low-altitude threats and served as a foundation for subsequent Sea Sparrow versions.

SPECIFICATIONS:
Guidance: Semi-active radar homing (monopulse seeker)
Warhead: 39 kg blast-fragmentation
Accuracy: All-aspect, look-down/shoot-down capable with ECCM
Length: 3.66 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 231 kg
Platforms: Mk 29 GMLS, Mk 41 VLS, Mk 48 VLS

Range: Approximately 19 km
Speed: Mach 2.5
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: 1983
Operators: United States, NATO member navies
Combat Use: Deployed for ship self-defense; specific combat engagements are not widely documented
Interesting Fact: The RIM-7M's enhancements over previous models improved naval defense against low-flying threats, setting the stage for subsequent Sea Sparrow advancements.

SOURCES:
U.S. Navy Fact File: https://www.navy.mil/Resources/Fact-Fil ... ile-rim-7/
Weaponsystems.net: https://weaponsystems.net/system/1391-R ... %2BSparrow
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

----- RIM-7P Sea Sparrow || Weapon_1003 ----------

OVERVIEW: The RIM-7P Sea Sparrow is a ship-launched, short-range, semi-active radar-guided surface-to-air missile, adapted from the AIM-7P Sparrow air-to-air missile. It incorporates mid-course guidance updates and improved low-altitude intercept capabilities, enhancing naval air defense.

DETAILS: Introduced in the early 1990s, the RIM-7P is a naval variant of the AIM-7P Sparrow III, integrated into the Mk 29 Guided Missile Launching System (GMLS). The missile features a digital guidance system capable of receiving mid-course updates via rear-mounted antennas, allowing for improved accuracy and flexibility in target engagement. Its warhead is a 39 kg blast-fragmentation type, designed to effectively engage high-speed aerial targets. The RIM-7P employs a semi-active radar homing guidance system, requiring continuous illumination of the target by the ship's radar. This variant offered enhanced performance against low-altitude threats and served as a foundation for the development of the Evolved Sea Sparrow Missile (ESSM).

SPECIFICATIONS:
Guidance: Semi-active radar homing with mid-course update capability
Warhead: 39 kg blast-fragmentation
Accuracy: All-aspect, look-down/shoot-down capable with ECCM
Length: 3.64 m
Diameter: 0.203 m
Wingspan: 1.02 m
Total Weight: 225 kg
Platforms: Mk 29 GMLS, Mk 41 VLS, Mk 48 VLS

Range: Approximately 19 km
Speed: Mach 2.5–3
Maneuverability: Up to 18 g in terminal phase

NOTES:
IOC: Early 1990s
Operators: United States, NATO member navies
Combat Use: Deployed for ship self-defense; specific combat engagements are not widely documented
Interesting Fact: The RIM-7P's enhancements over previous models improved naval defense against low-flying threats, setting the stage for the development of the Evolved Sea Sparrow Missile (ESSM).

SOURCES:
U.S. Navy Fact File: https://www.navy.mil/Resources/Fact-Fil ... ile-rim-7/
Weaponsystems.net: https://weaponsystems.net/system/1391-R ... %2BSparrow
Wikipedia: https://en.wikipedia.org/wiki/RIM-7_Sea_Sparrow

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Rams128 · Post by **Rams128** » Thu Jun 05, 2025 12:03 am

I created a general description for all used generic sensors. as they are clickable and linked to a proper database ID, but lack information. I believe this could benefit new players, and those who want a complete understanding, of every piece of equipment under their control, before starting a game, like myself. It also minimizes the need to search for Information on Google.

e.g. :
Generic MAWS
OVERVIEW: MAWS (Missile Approach Warning Systems) are defensive electronic systems designed to detect and alert aircrews to incoming missile threats, providing critical early warning to enable countermeasures deployment.

GENERAL DESCRIPTION: MAWS operate by passively detecting the ultraviolet (UV) or infrared (IR) signatures of incoming missiles during their launch and flight phases. These systems provide rapid threat identification and directional cues to the aircraft’s countermeasure dispensers, such as flares or DIRCM (Directional Infrared Countermeasures). MAWS are typically integrated into military aircraft, helicopters, and some UAVs to enhance survivability against man-portable and vehicle-launched surface-to-air missiles, as well as air-to-air missiles.

ROLE SUMMARY:
Category: Defensive Electronic Warfare / Missile Warning
Primary Use: Early detection and warning of incoming missile threats
Function: Passive IR/UV missile plume detection and threat direction cueing
Platform: Installed on military fixed-wing aircraft, helicopters, and UAVs

See Specific information under [Sensors/EW] and [Properties] sections.

SOURCE:
Federation of American Scientists (FAS)
Defense Industry Publications

Here are all the Descriptions (283 files).

Rams128 · Post by **Rams128** » Thu Jun 05, 2025 2:36 am

CV60 wrote: Mon Jun 02, 2025 6:47 pm Rams-Tank you very much for these. I'll get them in the next update!

It's a pleasure to contribute.

The ones I posted earlier for easy access:
(AMRAAMs - Pyhtons - SPICs - KABs - Sparrows)

CV60 · Post by **CV60** » Thu Jun 05, 2025 2:42 pm

Thank you. I'll also get these generic descriptions in the next update!

Rams128 · Post by **Rams128** » Thu Jun 05, 2025 7:29 pm

All used Generic Weapons.

e.g.:
Depth Charges [Generic]

OVERVIEW: Depth charges are anti-submarine weapons designed to detonate underwater at predetermined depths to damage or destroy submerged submarines through shock waves and pressure effects. They are typically deployed by surface ships, aircraft, or helicopters.

DETAILS: A depth charge consists of a cylindrical metal casing filled with high explosives such as TNT or Torpex and uses hydrostatic fuzes or time-delay mechanisms to trigger detonation at a specific depth. Upon detonation, the rapid release of energy creates a powerful pressure wave that can rupture submarine hulls or damage critical systems even without a direct hit. Depth charges are deployed individually or in patterns to saturate an area where a submarine is believed to be operating. They are a staple of naval anti-submarine warfare, particularly in close-range engagements.

ROLE SUMMARY:
Category: Anti-Submarine Warfare Munition
Primary Use: Anti-submarine
Function: Underwater explosive detonation at preset depths
Strong Against: Submarines at shallow to medium depths
Weak Against: Deep-diving submarines, fast-moving subs, surface ships, evasive targets
Platform: Naval vessels, maritime patrol aircraft, ASW helicopters
Integration: Compatible with depth charge racks, throwers, and aerial dispensers

SOURCE:
Janes Naval Weapon Systems
https://en.wikipedia.org/wiki/Depth_charge

Here are all the Descriptions (83 Files):

Rams128 · Post by **Rams128** » Fri Jun 06, 2025 10:11 am

Please Use this version for Generic Sensors.

CV60 · Post by **CV60** » Sat Jun 07, 2025 7:56 pm

Rams128 wrote: Fri Jun 06, 2025 10:11 am Please Use this version for Generic Sensors.

Will do. I'm packaging these all up this week for submission

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