Accession Number : AD0467569
Title : SYSTEM EFFECTS ON PROPELLANT STORABILITY AND VEHICLE PERFORMANCE.
Descriptive Note : Quarterly rept. no. 1, 3 May-23 Jul 65.
Corporate Author : DOUGLAS AIRCRAFT CO INC SANTA MONICA CA MISSILE AND SPACE SYSTEMS DIV
Report Date : 23 Jul 1965
Pagination or Media Count : 137
Abstract : The objective of this 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 having the general features itemized in Table I and the duty cycles covered in Table II. The approach that will be 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 coordinate with RPL personnel to implement this test plan; and (4) use the test results to appropriately modify the analytical models and reoptimize the vehicle design parameters where necessary. This approach shall be implemented by a nine-phase program as summarized below. (Author)
Descriptors : LIQUID ROCKET PROPELLANTS , SPACE PROPULSION , FEASIBILITY STUDIES , PERFORMANCE(ENGINEERING) , LIQUEFIED GASES , HYDROGEN , FLUORINE , LIQUID PROPELLANT ROCKET ENGINES , FEED PUMPS , FUEL INJECTORS , PROPELLANT CONTROL , PRESSURE , MATHEMATICAL MODELS , THERMAL INSULATION , AIRFRAMES , HEAT SHIELDS , RESEARCH MANAGEMENT
Distribution Statement : APPROVED FOR PUBLIC RELEASE