Free-Flight Test of a Technique for Inflating an NASA 12-Foot-Diameter Sphere at High Altitudes
Project G.A.S.P. Shaft Launching Facilities
Structural Considerations of Inflatable Reentry Vehicles
Analysis of Trajectory Parameters for Probe and Round-Trip Missions to Venus
Landing Energy Dissipation for Manned Reentry Vehicles
Effect of Load-Alleviating Structure on the Landing Behavior of a Reentry-Capsule Model
Analog Simulation of a Pilot-Controlled Rendezvous
Aerospace Structures Research and Development