[LOGGED] Request: Revise AAW missile max/avg speeds at lower altitudes
Posted: Sun Mar 08, 2026 1:45 pm
MOD: Continuation of discussion from here: https://forums.matrixgames.com/viewtopic.php?p=5266605
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Well, I would personally disagree with that 475kts (mere 0.72M, and should be around 1.5M) but it's a game design decision.
If you are interested in some real world data regarding to AIM-9L/M performance, here is is:
This is real world test data of standard AIM-9L Sidewinder compared to some experimental variant of it (with different nosecone). As you can see when launched at sea level, platform speed M0.9 (around 975ft/s, 577kts) AIM-9L accelerates to around 2700ft/s which is 823m/s, 1599kts, Mach 2.5.
Speed gain due to motor action is 1599-577=1022kts = ~Mach 1.6. Launched from stationary helo (or a ground launcher like Chapparal) it should reach a higher speed than 1022kts, as it would be less affected by drag when accelerating.
Rough calculations of missile/fuel mass and motor data with some ballistic software give results of a bit over Mach 2 for stationary launch at sea level (and almost Mach 2.5 theoretically without any air drag).
A Chapparal MIM-9 missiles are usually credited with at least Mach 1.5 speed (sometimes as Mach 2.5 but it's probably wrong number taken from air-launched AIM-9 data).
Reading from the graph again, max speed of AIM-9L launched at alt of 20kft at 0.9M is about 3200ft/s = 975m/s = 1895kts = 3.07M. This means delta V of 658m/s = ~2M = 1278kts. At 30-40ktf altitude speed would be even bit higher, bit closer to theoretical no-drag value.
The other very interesting thing in those graphs are the velocity profiles, which may be used to asses how realistic DLZ calculations are.
In second .7z attachement is same graph plus AIM-9L motor data and example real life DLZ data (10kft 0.9M) for AIM-9L.
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Well, I would personally disagree with that 475kts (mere 0.72M, and should be around 1.5M) but it's a game design decision.
If you are interested in some real world data regarding to AIM-9L/M performance, here is is:
This is real world test data of standard AIM-9L Sidewinder compared to some experimental variant of it (with different nosecone). As you can see when launched at sea level, platform speed M0.9 (around 975ft/s, 577kts) AIM-9L accelerates to around 2700ft/s which is 823m/s, 1599kts, Mach 2.5.
Speed gain due to motor action is 1599-577=1022kts = ~Mach 1.6. Launched from stationary helo (or a ground launcher like Chapparal) it should reach a higher speed than 1022kts, as it would be less affected by drag when accelerating.
Rough calculations of missile/fuel mass and motor data with some ballistic software give results of a bit over Mach 2 for stationary launch at sea level (and almost Mach 2.5 theoretically without any air drag).
A Chapparal MIM-9 missiles are usually credited with at least Mach 1.5 speed (sometimes as Mach 2.5 but it's probably wrong number taken from air-launched AIM-9 data).
Reading from the graph again, max speed of AIM-9L launched at alt of 20kft at 0.9M is about 3200ft/s = 975m/s = 1895kts = 3.07M. This means delta V of 658m/s = ~2M = 1278kts. At 30-40ktf altitude speed would be even bit higher, bit closer to theoretical no-drag value.
The other very interesting thing in those graphs are the velocity profiles, which may be used to asses how realistic DLZ calculations are.
In second .7z attachement is same graph plus AIM-9L motor data and example real life DLZ data (10kft 0.9M) for AIM-9L.