Rocket stabilisers

Details Rocket stabilisers Rocket stabilisers

F - Mech Eng,Light,Heat,Weapons

42

B

102/5, 60/73

F42B 10/12 (2006.01)

Patent

CA 1267035

ABSTRACT OF THE DISCLOSURE A rocket stabiliser is described for a rocket having a nozzle with an axi-symmetric exit lip, wherein an annular aerofoil is arranged in flight to be axially aligned with and axially spaced downstream from the exit lip, the aerofoil having an inner surface or greater flow path length than that of its outer surface. The stabilizer functions to move the centre of pressure rearwards. The stabiliser is particularly applicable to tube launched rockets.

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