Control of Chilldown and Pressure Rise in SF-1 Cruiser Tank and Transfer Line.
GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
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The objective of this test is to establish an optimum chilldown procedure for the SF-1 Transfer Line and Cruiser Tank, utilizing a minimum amount of SF-1 and the minimum time without exceeding the safe missile fuel tank operating pressure 11 psig and boiloff valve capability. Author
- Liquid Rocket Propellants
- Ground Support Systems and Facilities for Space Vehicles