Free-Flight Test of a Technique for Inflating an NASA 12-Foot-Diameter Sphere at High Altitudes
Structural Considerations of Inflatable Reentry Vehicles
Simulation of Structural Dynamics of Space Vehicles During Launch
Large Astronomical Satellite First Estimation of Thermal Distortions in a Stable Platform
Study for Passive Gravity Stabilization Final Technical Report, Jul. 1967 - Mar. 1968
A Lightweight 6 1/2-Ft Aeroshell for an Early MARS Probe Mission
Thermal Analysis of Small Cylindrical Ammonia Evaporators