Hydrogen Tankage Application to Manned Aerospace Systems, Phases II and III. Volume III. Structural Acceptance and Flight Simulation Testing
1968
200 pages
Report
Keine Angabe
Englisch
Manufacturing Processes & Materials Handling , Aircraft , Manned Spacecraft , Hypersonic aircraft , Propellant tanks , Performance(Engineering) , Flight testing , Simulation , Structural properties , Thermal properties , Leakage(Fluid) , Military requirements , Instrumentation , Thermal stresses , Thermal stability , Pressurization , Correlation techniques , Thermal insulation , Hypersonic characteristics , Test equipment , Cold weather tests , Hydrogen , Alloy 718 , Siamese configuration , Skin(Structural member) , S/L change 8323
Liquid hydrogen tankage design
NTRS | 1978
|NTRS | 1969
|Testing of manned flight systems
NTRS | 1963
HYDROGEN TANKAGE FOR HYPERSONIC CRUISE VEHICLES
AIAA | 1966
|