The patent describes a control system for supplying uncured propellant into the combustion chamber 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. (Author)
Thrust Management Control Propulsion System
1975
3 pages
Report
Keine Angabe
Englisch
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Europäisches Patentamt | 2024
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