Thrust management control propulsion system

Details Thrust management control propulsion system Thrust management control propulsion system

1975-10-03

1977-09-13

Croyle, Carlton R.

Power plants

Reaction motor

Gel propellant

60258, 251 635, 251120, 251332, 251340, F02K 904, F16K 31126

Patent

active

040473821

ABSTRACT:
A control system for supplying uncured propellant into the combustion char of a missile. The system includes a moving injector cooperating with a pressurized putty-like uncured propellant. This combination provides the missile with a propulsion system having rapid wide range throttling, shut off and restart capabilities.

REFERENCES:
patent: 2810259 (1957-10-01), Burdett
patent: 3064903 (1962-11-01), Butler
patent: 3098625 (1963-07-01), Thielman
patent: 3126701 (1964-03-01), Henderson et al.
patent: 3131906 (1964-05-01), King
patent: 3158994 (1964-12-01), Hodgson
patent: 3173252 (1965-03-01), Ziegenhagen
patent: 3232049 (1966-02-01), Rhodes
patent: 3349563 (1967-10-01), Taylor et al.
patent: 3908364 (1975-09-01), LeFebvre et al.

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