I will leave it to you to work out the designs of 'lifting body' a wing and wing size needed, There is a lot to itIsn't bigger fins means more drag hence much higher energy bleed during any manures ?
And how (in case of ASRAAM) , a cylinder body is able to generate enough lift ?
And do you know the advantage and disadvantage of fins like in Astra, Mica(or SM 3/6), Aim 120 and no fins llke Aim 260.
Like all 3 have very different fins, which is better in which case ?
And do you think/know that , Aim 260 will be menurable enough to take on fighter jet with target >200km ?
And how you see Astra Mk3, Aim 260 and PL-16 ? Like which one will be better at long distances against fighter jet ?
And is the air intake of Astra Mk3 or meteor has any nagative effect except for extra weight ? Like reduced menurabality ? Or reduced effect at less altitude ?
(I know very little about air to air missiles, that's why i asked, and if you have any good materials/videos on BVR A2A missiles and combat that i would love to read that)
The body lift asraam I gave as another method of control, was just for information on designs
The AIM-9X has wings
Ai
- Fuselage as a Wing: Instead of relying on large wings, the missile’s body is shaped to generate lift when flown at an angle of attack (tilted slightly relative to the oncoming air).
- Tail Control: ASRAAM relies on small control fins at the tail to pitch or yaw the missile. By adjusting these tail fins, the missile pivots its entire body into the airflow, allowing the main body to create massive amounts of aerodynamic lift.
- The missile is designed to be inherently unstable, meaning it naturally wants to pitch off-course. Its computer-controlled autopilot constantly adjusts the tail fins to maintain or alter the flight path, resulting in ultra-fast reaction times and extreme turn rates
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