Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
Inventor
active
Antirotation linkage for rocket motor nozzles and other mechanis
Energy absorber for translating portions of rocket motor cases u
Low friction, movable, rocket nozzle
Method for explosively forming an auxiliary exit cone for the no
Reduced fin span thrust vector controlled pulsed tactical missil
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Profile ID: LFUS-PAI-P-581968