Hi community,
here are some suggestions regarding KC-135 entries.
First and foremost, please note that everything below comes from books or websites, I have no first hand experience in the air, I did my best to double check things though.
So what you do have here is nothing more than pure research, nor nothing less. In other words, I've done my homework but it's all from public sources.
Sources:
- Boeing Kc-135 Stratotanker: More Than Just a Tanker (Aerofax Series, 1998), Robert S. Hopkins III, ISBN: 978-1857800692
- Jane's Aircraft Upgrades 2002-2003
- Flight International 14, November 1990
- International Air Power Review, Vol. 10, January 2003
- Allied Tactical Publication – 56(B) - Air to Air Refuelling, August 2011
-
http://www.defense.gouv.fr/air/
-
http://groupe-bretagne.fr/
-
http://www.ervc135-amicale.fr/
-
http://boeing.mediaroom.com/
-
http://www.peetz.us/kc135.htm
[*]
#1852 - KC-135A Stratotanker -- United States (Air Force), 1958-1993
Take-off/Landing Distance: should be 2601-3200m TOD/LAD (actual take-off run is 2760 m long).
Max Weight: should be 136800 kg.
Crew: should be 4 (pilot, co-pilot, boom operator, navigator).
Fuel Quantity: should be 88452 kg.
[*]
#1857 - KC-135F Stratotanker -- France (Air Force), 1965-1988
Name: is C-135F (the logic behind it would be that with its reinforced floor, it qualifies as Cargo and Transport aircraft too).
Date: First delivered C-135F came in February 1964, the last one in October 1964.
Take-off/Landing Distance: should be 2601-3200m TOD/LAD (actual take-off run is 2760 m long).
Max Weight: should be 136800 kg.
Crew: should be 4 (pilot, co-pilot, boom operator, navigator).
Sensors: should be a #2678 - AN/APN-59.
Stores: should add "Cargo [No Drop, 32 tons]", "Passenger" along the Tanker one, Cargo [No Drop, 19 tons], or 126 passengers, or a Medevac.
Loadout: should add "Cargo, 32 tons", "Passenger" along the Tanker one, Cargo [No Drop, 19 tons], "Passengers, 126x", or a Medevac.
Fuel Quantity: should be 81845 kg. (upper deck tank is not fitted, 6607 Kg less)
Note: #376 - Adelie -- KC-135F/FR
"Adèle" (not Adèlie), by Dassault Electronique "is a Radar Warning Receiver installed from 1990 on a single airframe that may have been deployed during Desert Storm". Examination of C-135F pictures led me to the conclusion that Adèle haven't been anymore since.
[*]
#782 - KC-135FR Stratotanker -- France (Air Force), 1985-0
Name: is C-135FR (R for "Remotorisé")
Date: 1985-1994 (please see new entry proposal below).
Take-off/Landing Distance: should be 2601-3200m TOD/LAD (actual take-off run is 2760 m long).
Crew: should be 4 (pilot, co-pilot, boom operator, navigator).
Sensors: should be a #2678 - AN/APN-59, see abive about Adèle.
Stores: should add "Cargo [No Drop, 32 tons]", "Passenger" and "Casualty" along the Tanker one.
Loadout: should add "Cargo, 32 tons", "Passenger" along the Tanker one, Cargo [No Drop, 19 tons], "Passengers, 126x", or a Medevac.
Military Static Thrust at S/L: should be 10044 kg per engine.
Fuel Quantity: should be 85604 kg. (upper deck tank is not fitted, 6607 Kg less)
[*]
#159 - KC-135E Stratotanker -- United States (Air Force), 1982-2006
Max Weight: should be 136800 kg.
Crew: should be 4 (pilot, co-pilot, boom operator, navigator).
Military Static Thrust at S/L: should be 8219 kg per engine.
Fuel Quantity: should be 88452 kg.
[*]
#1320 - KC-135Q Stratotanker -- United States (Air Force), 1966-1995, SR-71 JP-7
Take-off/Landing Distance: should be 2601-3200m TOD/LAD (actual take-off run is 2760 m long).
Max Weight: should be 136800 kg.
Crew: should be 4 (pilot, co-pilot, boom operator, navigator).
Fuel Quantity: should be 83684 kg. ("The KC-135Q can simultaneously carry a maximum of 33,788kg of JP-7 and 49,896kg of standard JP-4.")
[*]
#1692 - KC-135R Stratotanker -- United States (Air Force), 1984-0
Military Static Thrust at S/L: should be 10044 kg per engine.
Fuel Quantity: should be 92211 kg.
[*]
#1984 - KC-135R Stratotanker -- United States (Air Force), 1997-0
Military Static Thrust at S/L: should be 10044 kg per engine.
Fuel Quantity: should be 92211 kg.
Loadout: should have a Tanker [Wing Drogue & Centerline Boom]
[*]
#1854 - KC-135R Stratotanker -- Singapore (Air Force), 2000-0
Military Static Thrust at S/L: should be 10044 kg per engine.
Fuel Quantity: should be 92211 kg.
Loadout: should have a Tanker [Wing Drogue & Centerline Boom]
[*]
#1853 - KC-135R Stratotanker -- Turkey (Air Force), 1999-0
Military Static Thrust at S/L: should be 10044 kg per engine.
Fuel Quantity: should be 92211 kg.
Note: to the best of my knowledge, they have no Wing Drogue capacity.
[*]
#808 - KC-135T Stratotanker -- United States (Air Force), 1995-0, Special Fuel
Military Static Thrust at S/L: should be 10044 kg per engine.
Fuel Quantity: should be 92211 kg.
Note: Jane's Aircraft Upgrades claim that it's the "Only KC-135s capable of receiving fuel" but I haven't found any other source to support that statement.
New platforms proposal:
[*]
#### - KC-135E Stratotanker -- Chile (Air Force), 2010-0
Chile bought 3 of them (57-1501, 58-0014 and probably 57-2594). First delivered in February 2010, second in August 2011 and third in March 2012.
[*]
#### - C-135FR Stratotanker -- France (Air Force), 1994-0
Loadout: should have a Tanker [Wing Drogue & Centerline Boom]
Properties: add Wing Drogue
Otherwise, copy #782 (with suggested changes above)
[*]
#### - KC-135R Stratotanker -- France (Air Force), 1997-0
3 acquired (497, 525, 574), first delivered in June 1997. Copy #1692 - KC-135R (with suggested changes above).
Hope it helps.