Precision controlled variable thrust solid propellant rocket...

Details Precision controlled variable thrust solid propellant rocket... Precision controlled variable thrust solid propellant rocket...

2011-06-14

2011-06-14

Ellis, Christopher P (Department: 3644)

Power plants

Reaction motor

Method of operation

C244S003220, C102S374000, C060S229000

Reexamination Certificate

active

07958718

ABSTRACT:
A multiple-stage solid rocket motor is operated in a manner designed to control its mass discharge profile. This is accomplished by providing means for igniting one stage and then igniting a subsequent stage while the first continues to burn.

REFERENCES:
patent: 2856851 (1958-10-01), Thomas
patent: 3044255 (1962-07-01), Precoul
patent: 3274772 (1966-09-01), Hawkins et al.
patent: 3688636 (1972-09-01), Spiess et al.
patent: 3712058 (1973-01-01), Cooper
patent: 4223606 (1980-09-01), Bornstein
patent: 4817377 (1989-04-01), Kirschner, Jr. et al.
patent: 4840024 (1989-06-01), McDonald

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