Flexible Integrated Solar Cell Array
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
An Investigation of Leakage of Large-Diameter O-Ring Seals on Spacecraft Air-Lock Hatches
A Study of Aseptic Maintenance by Pressurization
An Investigation of APOLLO Titanium Pressure Vessel Welds Made with Commercially Pure Filler Wire
Thermal Analysis of Small Cylindrical Ammonia Evaporators
Development of Energy-Dissipating Plastic Honeycomb Final Report
Proceedings of the 3RD Aerospace Mechanisms Symposium
Staging Loads - Space Vehicle Design Criteria
Study of Structural-Thermal Insulation- Meteoroid Protection Integration
Integral Launch and Reentry Vehicle. Volume 2 - Technology Identification Final Report