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).
Reusable Subsystems Design/Analysis Study. Volume 2. Part A. Technical Study Report
1970
302 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Manned Spacecraft , Space Launch Vehicles & Support Equipment , Liquid rocket propellants , Cryogenic propellants , Recoverable booster motors , Spacecraft , Storable rocket propellants , Space probes , Recovery , Selection , Design , Space shuttles , Reusable spacecraft , Cryogenic spacecraft , Propellant utilization , Fdl-5 vehicles , Tradeoffs , Storable spacecraft