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
Aerospace Expandable Structures
The Prediction of Inflight Dynamic Stresses in Typical Spacecraft Shell Structures
Space Craft Soft Landing System
Effect of Power Dissipation on the Platform Temperatures of the L.A.S
Simulation of Structural Dynamics of Space Vehicles During Launch
Thermal Control of Space Vehicles
Structure and Materials Aspects of the Prime Flight Test Vehicle
Aerodynamic Deployable Decelerator Performance - Evaluation Program
The Extra Vehicular Manufacture of Large Space Structures from Storable Tubular Members
Large Astronomical Satellite First Estimation of Thermal Distortions in a Stable Platform
Protective Structures and Components: Compilation of Abstracts
Investigation of Independent Structure (Space) Crew Escape Concepts
Structural Design Concepts for Variable-Geometry Lifting Surfaces of Reentry Vehicles
Environmental Test Contribution to Spacecraft Reliability
First Estimation of Weights for the L.A.S. And Specific Weights of Satellites
Review of Beryllium Technology for Spacecraft Applications
Review of Advanced Composite Materials for Spacecraft Applications
Triaxial Balancing Problems. San Marco 2 Satellite Balancing
Milestone Report of a Study of Space Mission Duration Extension Problems, Volume 2
Flexible Integrated Solar Cell Array
Dynamic Stability of Space Vehicles. Volume 12 - Re-Entry Vehicle Landing Ability and Control
The Black Arrow X3 Spacecraft Structure
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
Stability of Structural Materials for Spacecraft Application Final Report
An Investigation of Leakage of Large-Diameter O-Ring Seals on Spacecraft Air-Lock Hatches
Reusable Transport System - Neptun Mass-Model
Deployment of Spacecraft Appendages and Temperature Control of Experiments Final Technical Report