Propulsion system

Power plants – Reaction motor – Liquid oxidizer

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Details

244 323, F02K 902

Patent

active

042585465

ABSTRACT:
A liquid rocket propulsion system utilizing vehicle spin forces and/or propellant tank pressure to charge a specific amount of propellant through a differential area piston to create high chamber pressure.

REFERENCES:
patent: 2410538 (1946-11-01), Walton
patent: 2918791 (1959-12-01), Greiner
patent: 3011312 (1961-12-01), Black
patent: 3088406 (1963-05-01), Horner
patent: 3479818 (1969-11-01), Strobl
Traynelis et al., "Study of Integrated Control Systems," ASD Tech. Rpt. pp. 61-327, vol. 1, Nov., 1961, Sect. 2.2.

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