Combustion suppressor

Details Combustion suppressor Combustion suppressor

1980-10-06

1983-02-15

Brown, David H.

Ordnance

Rocket launching

Having safety devices for preventing premature ignition or...

89 1817, F41F 304

Patent

active

043734200

ABSTRACT:
Method and apparatus for preventing combustion of exhaust gases in rocket launch systems using a plurality of launch tubes connected to a plenum including pressure sensors in each launch tube, a control system sensitive to atmospheric pressure and launch tube pressure which provides a signal to an inert gas supply flow controller to initiate flow of gas into the plenum when pressure in a launch tube, after launch of a rocket, reaches a predetermined level.

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