Post boost control power assembly

Details Post boost control power assembly Post boost control power assembly

2011-01-25

2011-01-25

Gregory, Bernarr E (Department: 3662)

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

C244S00100R, C244S003100, C244S003150, C244S003210, C244S158100, C244S164000, C244S169000

Reexamination Certificate

active

07875838

ABSTRACT:
A tubular distributor in a missile having a right-angled hollow tubular first section, the right-angled hollow tubular first section having a first leg and a second leg, a straight hollow tubular second section, an end of the first leg of the right-angled hollow tubular first section perpendicularly connected to a first end of the hollow tubular second section, a straight hollow tubular third section, a first end of the hollow tubular third section perpendicularly connected to the first end of the straight hollow tubular second section, and a close/open valve positioned within the straight hollow tubular third section, the close/open valve positioned between a gas generator and the straight hollow tubular second section.

REFERENCES:
patent: 3645475 (1972-02-01), Stripling
patent: 3736749 (1973-06-01), Kretschmer et al.
patent: 4550888 (1985-11-01), Douglass et al.
patent: 5062593 (1991-11-01), Goddard et al.
patent: 5111553 (1992-05-01), Muggeridge et al.
patent: 7118065 (2006-10-01), Heitmann et al.
patent: 7416154 (2008-08-01), Bittle et al.

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