The objective of the program is to study the influence of pertinent system design features and parameters on propellant storability and vehicle performance for a hypothetical LF2/LH2 maneuvering space propulsion system. The approach taken is to (1) perform theoretical studies on each basic sub-system and use the resulting data to optimize critical parameters for the overall system; (2) design and fabricate a test apparatus for evaluating as completely as possible, in a space simulation chamber, the analytical models used and the appropriate influence coefficients for inclusion into these models; (3) evolve a test plan for utilizing this test apparatus; and (4) use the test results to appropriately modify the analytical models and reoptimize the vehicle design parameters where necessary.
System Effects on Propellant Storability and Vehicle Performance
1965
146 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Rocket Propellants , Rocket motors(Liquid propellant) , Space propulsion , Liquid rocket propellants , Performance(Engineering) , Systems engineering , Storage , Feasibility studies , Liquefied gases , Hydrogen , Fluorine , Theory , Feed pumps , Fuel injectors , Propellant control , Pressure , Venting , Pressurization , Models(Simulations) , Mathematical models , Thermal insulation , Airframes , Design , Heat shields , Research program administration , Space simulation chambers
Propellant Storability in Space
NTIS | 1964
|Long-Term Storability of Propellant Tankage
NTIS | 1971
|Storability of fuming nitric acid
NTRS | 1953
|