Rocket catapult with direct mechanically actuated ignition of ro

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

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Details

89 1816, 244122AB, B64D 2510

Patent

active

040364569

ABSTRACT:
An improved rocket catapult is disclosed for use in aircraft ejection systems permitting direct ignition of the rocket motor by a mechanically-actuated igniter situated in proximity to the rocket motor grain and which is actuated when the rocket motor has traveled a predetermined distance during the catapult phase of its operation.

REFERENCES:
patent: 2954947 (1960-10-01), Zabelka et al.
patent: 3126177 (1964-03-01), Markowitz

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