Active control of solid propellant generators using throat modul

Details Active control of solid propellant generators using throat modul Active control of solid propellant generators using throat modul

1982-06-01

1990-02-06

Kyle, Deborah L.

Power plants

Reaction motor

Condition responsive thrust varying means

60254, F02K 118

Patent

active

H00007471

ABSTRACT:
A system for controlling solid propellant gas generators including a microcessor which has inputs such as the sensed temperature of the gases in the solid propellant gas generator, the pressure within the solid propellant gas generator and/or pre-programmed input control signals to the microprocessor for causing the microprocessor to produce signals that are used to control a modulation valve which in turn controls a thrust nozzle device that controls exhaust gases from the solid propellant gas generator.

REFERENCES:
patent: 3030769 (1962-04-01), Badders
patent: 3059425 (1962-10-01), McSherry et al.
patent: 3073112 (1963-01-01), Blelkamp, Jr.
patent: 3626697 (1971-12-01), Nunn et al.
patent: 3641766 (1972-02-01), Uehling
patent: 3759039 (1974-09-01), Williams
patent: 3948042 (1976-04-01), Beardsley et al.
Sutton et al., Rocket Propulsion Elements, 1976, pp. 358-364.

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