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).


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    Title :

    Reusable Subsystems Design/Analysis Study. Volume 2. Part A. Technical Study Report


    Contributors:

    Publication date :

    1970


    Size :

    302 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English