Rocket catapult

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244122AD, B64D 2510

Patent

active

039790886

ABSTRACT:
A rocket catapult ejection system for a seat-occupant mass of a disabled craft in which the rocket motor has an annular nozzle throat defined by a spherical pintle and an adjustable nozzle housing. Axial adjustment of the nozzle housing will displace the centroid of the nozzle throat and adjust the rocket thrust vector to compensate for deviations in the occupant-seat mass center of gravity.

REFERENCES:
patent: 3735948 (1973-05-01), MacDonald et al.

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