This report is the vehicle preliminary design data portion of Phase I and basically provides a definition of a vehicle and mission, developes a structural design criteria by examination of the overall system requirements and finally, provides data for the Phase II engineering effort, within the limits described by AFLC. (Author)
High Temperature, Stressed Skin Airframe Structure Development Program. Vehicle Preliminary Design
1959
161 pages
Report
No indication
English
Manned Spacecraft , Structural Mechanics , Fluid Mechanics , Lifting reentry vehicles , Airframes , Structural properties , Reentry vehicles , Nonpowered flight , Ascent trajectories , Descent trajectories , Aerostatics , Aerodynamic characteristics , Stability , Lift , Drag , Aerodynamic heating , Loads(Forces) , Controlled atmospheres , Auxiliary power plants , Sandwich construction , Cobalt alloys , Nickel alloys , Hypersonic aircraft , Thermal insulation , Experimental design , Graphs(Charts) , Skin(Structural member)
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