System, developed to provide control at high altitudes in regions of low dynamic pressure and to operate at zero normal acceleration and in extremely low-temperature environment, consists of storage vessel, pressurization system, flow control system, and rocket units; on-off control is used with which rockets are operated at fixed thrust levels of from 20 to 40 lb; problems encountered, fabrication of system, and data pertinent to performance characteristics.
Hydrogen-peroxide rocket reaction-control system for X-1b research airplane
NASA -- Tech Note
1959
28 pages
Report
English
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