Two-way rocket plenum for combustion suppression

Details Two-way rocket plenum for combustion suppression Two-way rocket plenum for combustion suppression

1977-12-12

1979-11-13

Brown, David H.

Ordnance

Rocket launching

Method of making

89 1816, F41F 304

Patent

active

041739191

ABSTRACT:
A system utilizing a rocket plenum design which is of a form to reduce and control combustion therein. The plenum is provided with two oppositely and upwardly extending exhaust ducts. Provision is made to eliminate blind pockets and stagnation passages in order to prevent possible explosions in the plenum during rocket firing.

REFERENCES:
patent: 2445423 (1948-07-01), Eastman
patent: 2925013 (1960-02-01), Santora et al.
patent: 2987964 (1961-06-01), Logan et al.
patent: 2998754 (1961-09-01), Bialy
patent: 3226063 (1965-12-01), Wagner
patent: 3228294 (1966-01-01), Hickman
patent: 3228296 (1966-01-01), Neuman et al.
patent: 3363508 (1968-01-01), Stahmer
patent: 4044648 (1977-08-01), Piesik

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