This volume provides supplemental data by way of appendixes to the task presented in Volume II AD-506 593, and AD-506 594. These appendixes include a Technology Summary, A Proposed Specification for Reusable Propulsion Components and Feed System, and Stress Analysis of Reusable Propellant Tanks. The Technology Summary presents a listing and information regarding previous technology programs in the areas of: integrated propulsion systems, cryogenic pressurization, cryogenic reaction control systems, propellant feed lines, liquid propellant tankage, propellant orientation and acquisition, inflight propellant conditioning, and space vehicle fluorine systems. The proposed specifications include a Proposed General Specification for Rocket Propulsion Fluid System Components and a Proposed General Specification for Rocket Propulsion Propellant Feed System, each obtained by modification of existing specifications. The stress analyses are presented for Reusable Launch Vehicle Propellant Tanks, Structural Analysis of Unsymmetric Fuel Tanks, and Symmetric Propellant Tanks.
Reusable Subsystems Design/Analysis Study. Volume 3. Supplemental Data
1970
165 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Manned Spacecraft , Space Launch Vehicles & Support Equipment , Liquid rocket propellants , Cryogenic propellants , Spacecraft , Recoverable booster motors , Design , Storable rocket propellants , Space probes , Recovery , Feed pumps , Leakage(Fluid) , Tank liners , Specifications , Pressure regulators , Asymmetric bodies , Propellant tanks , Liquid rocket oxidizers , Stresses , Reusable spacecraft , Cryogenic spacecraft , Space shuttles , Tradeoffs , Storable spacecraft