A Lightweight 6 1/2-Ft Aeroshell for an Early MARS Probe Mission
Stability of Structural Materials for Spacecraft Application Final Report
Reusable Transport System - Neptun Mass-Model
An Investigation of Leakage of Large-Diameter O-Ring Seals on Spacecraft Air-Lock Hatches
Deployment of Spacecraft Appendages and Temperature Control of Experiments Final Technical Report
A Study of Aseptic Maintenance by Pressurization
Thermal Analysis of Small Cylindrical Ammonia Evaporators
An Investigation of APOLLO Titanium Pressure Vessel Welds Made with Commercially Pure Filler Wire
Development of Energy-Dissipating Plastic Honeycomb Final Report
Proceedings of the 3RD Aerospace Mechanisms Symposium
Surveyor Surface Sampler Instrument