Study - Programming LOX Tank Pressure by Controlling the Regulator Sensing Line Pressure.
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
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The objective of this test was to investigate methods of programming a LOX tank airborne regulator so that a 26.0 psid maximum tank pressure would be maintained during the first twenty seconds of powered flight, and a 31.0 psid maximum pressure would be maintained during the remainder of the flight. Author
- Test Facilities, Equipment and Methods
- Liquid Rocket Propellants
- Ground Support Systems and Facilities for Space Vehicles