Afterburning reduction

Fire extinguishers – Processes – Of preventing fire

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Details

60264, 60266, 60 395, 169 62, 23926517, A62C 114, A62C 118, A62C 308

Patent

active

046306838

ABSTRACT:
A method of reducing the visible flash caused from afterburning of a rocket otor by injecting a fire extinguishing suppressant material into the exhaust gases from the rocket motor and injecting the fire extinguishing suppressant material near the exhaust end of the rocket motor nozzle and about an internal periphery of the exhaust nozzle. An effective fire extinguisher suppressant includes fluoro halogenated carbon compounds and specifically CBrF.sub.3.

REFERENCES:
patent: 2837891 (1958-06-01), Stasiak
patent: 3815360 (1974-06-01), Wellinitz
patent: 4113019 (1978-09-01), Sobolev et al.

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