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> What use is extreme maneuverability in a missile designed to engage helicopters?View attachment 24225View attachment 24226
VSHORAD is likely the only missile in its class with a reaction control system instead of the more common thrust vectoring, providing it with extreme maneuverability
> Even if you achieve extreme maneuverability, you're speed is still just Mach 1.5?
> Reaction control is generally used where there's no atmosphere to use traditional Control Surfaces like higher altitude or even space
> In endo-atmospheric role it's used when the speed is so high that the response from regular Control Surfaces would "lag" significantly like in case of PAC3-CRI with Mach 5 or Aster-30 with Mach 4.5
> After just a few meters from the launcher all the four divergent thrusters are fired (notice four separate plumes), so how can they be used later? And if there are multiple tandem motors inside then how much fuel are you actually going to pack inside a small missile?

> RCS thrusters are almost always placed perpendicular to the fuselage as that's the only way to use the total force to change the yaw or pitch. Also the thrusters are placed as further front as possible the lever arm is longest, generating maximum turning moment. If placed too close to the actual rear thrusters then it may cause the missile to "skid" instead of turning

>If placed tangentially then instead of the whole force, you'll get just the vertical component of it. In this case Fy which would always be smaller than force F as it'd be sin θ times of it

Someone should dig deeper into this and probably ask someone from DRDO (not from Adani, who's poster were first to claim this RCS thing)