Accession Number : AD0506593

Title :   Reusable Subsystems Design/Analysis Study. Volume II. Part A. Technical Study Report.

Descriptive Note : Final rept. Dec 68-Jul 69,

Corporate Author : LOCKHEED MISSILES AND SPACE CO SUNNYVALE CALIF

Personal Author(s) : Morgan,Lucian L. ; Gorman,R. L. ; Jensen,H. L. ; Hausman,R. F. ; Burbridge,H. K.

Report Date : JAN 1970

Pagination or Media Count : 302

Abstract : Contents: Vehicle Selection--Baseline Missions; Reusable VTOHL Space Launch Vehicles (LD2/LH2 propellants); Reusable Cryogenic Spacecraft (LF2/LH2 Propellants); Reusable Storable Spacecraft (N2O4/50-60 Propellants); Vehicle Design Extension--Engine operational requirements and modes, Propellant tankage, Propellant tank support, Pressurization subsystem evaluations, Attitude control subsystems, Propulsion subsystem schematics and definition, Propellant feedline systems, Propellant orientation, Propellant utilization systems, Thermal protection systems; Extension of Subsystem Analyses--Thermal analyses, Propulsion subsystem reentry hazards and effects, Passivation hazards and effects; Determination of Subsystem Requirements--Total active and inactive life requirements, acceptable propellant leak rates, Acceleration loading(G-vectors).

Descriptors :   (*LIQUID ROCKET PROPELLANTS, RECOVERABLE BOOSTER MOTORS), (*CRYOGENIC PROPELLANTS, SPACECRAFT), STORABLE ROCKET PROPELLANTS, SPACE PROBES, RECOVERY, SELECTION, DESIGN (U) *MANNED SPACECRAFT, LOGISTICS, THRUST, LIQUEFIED GASES, OXYGEN, HYDROGEN, NITROGEN OXIDES, TETROXIDES, PROPELLANT TANKS, FLUORINE, ATTITUDE CONTROL SYSTEMS

Subject Categories : Liquid Rocket Propellants
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE