Inert gas generants for utilization with rocket motors

Details Inert gas generants for utilization with rocket motors Inert gas generants for utilization with rocket motors

1973-10-02

1982-03-30

Walsh, Donald P.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

23926517, 23926525, B63H 1100

Patent

active

043220355

ABSTRACT:
Means for generating an inert enveloping gas for surrounding the exhaust me of a rocket motor are disclosed along with how the enveloping gas serves to prevent the adverse interaction between the rocket motor exhaust plume and the on-board sensors when the rocket motor is operating in exoatmospheric environments. Means for generating an inert enveloping gas utilizes a combination of a T-tube rocket motor and a donut of a chemical which is a gas generant selected from hydrazine bisborane, covalent azides, tetracene, or fluorocarbon-nitroamine.

REFERENCES:
patent: 3028807 (1962-04-01), Burton et al.
patent: 3091924 (1963-06-01), Wilder, Jr.

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