Lunar Return Reentry Thermal Analysis of a Generic Crew Exploration Vehicle Wall Structures
Low-Mass Inflation Systems for Inflatable Structures
LDR (Large Deployable Reflector) Structural Experiment Definition
Launch of the Meteoroid Technology Satellite
Large Solar Array Development in UK
Large Astronomical Satellite First Estimation of Thermal Distortions in a Stable Platform
Key Design Parameters for a Very Low Gravity in-Orbit Facility
James Webb Space Telescope Mission
Inflated Concepts for the Earth Science Geostationary Platform and an Associated Flight Experiment
Inflatable Re-Entry Vehicle Experiment (IRVE) Design Overview
Hypervelocity Impact Testing of L-Band Truss Cable Meteoroid Shielding on Skylab
HEEET: Innovative New TPS for Extreme Entry
Heatpipes and Vapor Chambers for Satellite Thermal Balance
From Apollo to Future Missions to Moon, Mars and Beyond - on Entry and Thermal Protection Systems
Free-Flight Test of a Technique for Inflating an NASA 12-Foot-Diameter Sphere at High Altitudes
Flight Performance of the Inflatable Reentry Vehicle Experiment 3