Method of launching a missile using secondary combustion

Details Method of launching a missile using secondary combustion Method of launching a missile using secondary combustion

1985-07-15

1987-06-09

Brown, David H.

Ordnance

Rocket launching

Underwater launching

89 1818, F41F 304

Patent

active

046711635

ABSTRACT:
In launching a missile from a launch tube, variable launch energy can be obtained by providing combustible products in the products of combustion from a gas generator and controlling the temperature and amount of oxygen present in the launch chamber to control the amount of secondary combustion in the launch chamber to provide a predetermined total launch energy and missile muzzle velocity.

REFERENCES:
patent: 2989899 (1961-06-01), Siegel et al.
patent: 3087386 (1963-04-01), Rung et al.
patent: 3088377 (1963-05-01), Siegel et al.
patent: 3137203 (1964-06-01), Brown
patent: 3182554 (1965-05-01), Barakauskas
patent: 3242810 (1966-03-01), La Pointe
patent: 3295411 (1967-01-01), Lehmann
patent: 3583277 (1971-06-01), Crockett
patent: 4185538 (1980-01-01), Barakauskas
patent: 4436016 (1984-03-01), Olmsted et al.

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