Accession Number : AD0511038
Title : Advanced Maneuvering Propulsion System (Lockheed Propellant Feed System Design). Volume III--Part A - Screening and Optimization Analyses.
Descriptive Note : Final rept. 1 Dec 67-31 Dec 69.
Corporate Author : ROCKETDYNE CANOGA PARK CALIF
Report Date : SEP 1970
Pagination or Media Count : 338
Abstract : Part A of this volume provides: the study ground rules and vehicle environments to which the propellant feed system is designed; a Configuration Optimization Study that allowed selection of the propellant tanks and shell; an impact study of an integrated attitude control system (F2/H2) as compared to the reference Compound A/MHF-5 attitude control system; and screening and optimization analyses that led to the design requirements for the external load-carrying shell, engine thrust structure, thermal control coating, engine actuators, tank support struts, insulation systems, ground hold vent-free oxidizer tank system and flight tank-pressure-control system.
Descriptors : (*LIQUID PROPELLANT ROCKET ENGINES, PROPELLANT CONTROL), THERMAL INSULATION, PROPELLANT TANKS, SHELLS(STRUCTURAL FORMS), COATINGS, OPTIMIZATION, VENTS, STRUCTURAL MEMBERS, PRESSURIZATION, SLOSHING, BAFFLES, THERMAL ANALYSIS, ACTUATORS, PRESSURE REGULATORS, HEAT EXCHANGERS (U) *CONTROLLABLE-THRUST ROCKET MOTORS, *CRYOGENIC PROPELLANTS, LIQUEFIED GASES, POLAR ORBIT TRAJECTORIES, ADVANCED WEAPONS, HYDROGEN, FLUORINE, MANEUVERING SATELLITES, ATTITUDE CONTROL SYSTEMS, SPACE ENVIRONMENTS, STARTING, MANEUVERABILITY, HYDRAZINE, METHYL HYDRAZINES, ASCENT TRAJECTORIES, FLUORIDES, CHLORINE COMPOUNDS
Subject Categories : Liquid Propellant Rocket Engines
Liquid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE