Rocket projectiles

Details Rocket projectiles Rocket projectiles

F - Mech Eng,Light,Heat,Weapons

42

B

60/41, 244/1.5

F42B 15/00 (2006.01)

Patent

CA 1244395

ABSTRACT OF THE DISCLOSURE A control system for a guided missile includes means for rotating the missile about its axis, a discharge nozzle so directed that its thrust exerts a lateral force on the missile and an associated reaction motor arranged to deliver, in response to a suitable signal, a thrust of suitable timing and duration to correct the missile trajectory. A suitable reaction motor has a combustion chamber in communication with the discharge nozzle by way of a relief valve, a compressible fuel tank pressurised by gases from the combustion chamber by way of a differential piston pump actuable by the combustion gases and controlled by a command operable, solenoid actuated valve, and means for initially heating and pressurising the combustion chamber.

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