Fuel Optimal Maneuver: Experimental Testbeds
Inmarsat Omni-Antenna Deployment Mechanism
A Lightweight 6 1/2-Ft Aeroshell for an Early MARS Probe Mission
Yuujin Gijutsu Shiken Eisei (Manned Engineering Test Satellites)
Study of Structural-Thermal Insulation- Meteoroid Protection Integration
Apollo Experience Report: Thermal Protection Subsystem
Integral Launch and Reentry Vehicle. Volume 2 - Technology Identification Final Report
Structural Dynamics and Control of Large Space Structures, 1982
Satellite Assembly in Geostationary Orbit: A Plug-and-Socket Concept
Third Conference on Fibrous Composites in Flight Vehicle Design, Part 2
Manned Orbital Systems Concepts Study. Book 5: User Analysis Supplemental Task
Personnel Occupied Woven Envelope Robot Power
Antenna Mechanical Technologies within ESA
JEM Development Status and Plan for JEM Crew Training
Space Shuttle Technical Conference. Part 1
Research and Technology Annual Report FY-1981
Getsumen Chakurikuki No Gainen Kentou (Conceptual Study of Lunar Landing Modules)
Space Tug Systems Study (Storable). Volume 1: Overview Presentation
Qualification Testing - Space Vehicle Design Criteria
Advanced Composite Structures At NASA Langley Research Center
Adaptive Structures Flight Experiments
Thermal Model of a 75 Watt/E/ Space Power Planar Rtg System
Structural Design of a Mobile Lunar Habitat With Multi- Layered Environmental Shielding
Advances in Design and Testing of Spacecraft Structures
Spacecraft Charge Build-Up Analysis
Space Operations Center System Analysis Study Extension. Volume 1: Executive Summary
Thruster Exhaust Effects Upon Spacecraft
Development of Deployable Structures for Large Space Platform Systems, Part 1
Space Launch System Mobile Launcher Modal Pretest Analysis
Spacecraft Dynamics and Control Program at AFRPL (Air Force Rocket Propulsion Lab)
MSAT Boom Joint Testing and Load Absorber Design
Space Station Program and Preliminary Design of JEM
Shuttle Considerations for the Design of Large Space Structures
Composite Technology for Exploration
The 7TH Aerospace Mechanisms Symposium
Modern Advances in Ablative TPS
Response of Flexible Space Vehicles to Docking Impact. Volume 2 - Numerical Investigation
Suitability of Various Spacecraft for Future Space Applications Missions
Calculation of the Penetration Flux for a Multiwall Structure on the Lunar Orbiter Spacecraft
Flight Testing of a Low Cost De-Orbiting Device for Small Satellites