Studies carried out for method of space vehicle attitude control using forces developed by hydrogen peroxide thrust chambers; propellant characteristics and physical properties of 90% H2O2; details of reaction control propulsion pressure-fed system wherein regulated helium pressure applied to positive expulsion monopropellant tank supplies H2O2 to thrust chambers, where rapid decomposition occurs; subsystems involved; 3 basic operating modes which employ each subsystem independently or in combination; results of program.
Mercury capsule reaction control propulsion system
Missiles Space
1962
Aufsatz (Zeitschrift)
Englisch
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