Rocket stabilizing apparatus

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Patent

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Details

244 33, F42B 1332

Patent

active

H00008540

ABSTRACT:
Apparatus for stabilizing the flight of a rocket wherein the body of the ket is provided with a plurality of petals arranged around the periphery of the aft end of the rocket with the leading end of each petal being pivotally attached to the rocket body such that the trailing end of each petal is free to move outward away from the rocket body. A ring slidably mounted on the rocket is linked to each of the petals in such a manner that as the ring moves in an aft direction on the rocket body the trailing ends of all of the petals simultaneously move outward equal distances from the rocket body.

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