Add to ORKGTests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
The comparative program costs associated with use of various standardized spacecraft for Air Force s...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...
Thermal and space environment simulation testing of Gemini extravehicular space sui
Voyager spacecraft and operation support equipment design and program planning for flight test missi...
Passive temperature control coatings for Apollo spacecraft ablative thermal protection syste
On April 5, 1983, an Inertial Upper Stage (IUS) spacecraft experienced loss of control during the bu...
The sixth Atlas Centaur vehicle (AC-6) was successfully launched from the Eastern T e s t Range, Com...
Heat and mass transfer, thermodynamics, fluid mechanics, and energy conversion studies for space fli...
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with...
The second task of a study with the overall objective of providing a conceptual definition of the Te...
The current technical effort is part of the third phase of a broad-scoped and systematic study of sp...
Design and fabrication of sterilization container and model probe assembly for Mars landing capsul
Water cascade heat pump system design and developed for continuous operation in thermal control syst...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
The comparative program costs associated with use of various standardized spacecraft for Air Force s...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...
Thermal and space environment simulation testing of Gemini extravehicular space sui
Voyager spacecraft and operation support equipment design and program planning for flight test missi...
Passive temperature control coatings for Apollo spacecraft ablative thermal protection syste
On April 5, 1983, an Inertial Upper Stage (IUS) spacecraft experienced loss of control during the bu...
The sixth Atlas Centaur vehicle (AC-6) was successfully launched from the Eastern T e s t Range, Com...
Heat and mass transfer, thermodynamics, fluid mechanics, and energy conversion studies for space fli...
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with...
The second task of a study with the overall objective of providing a conceptual definition of the Te...
The current technical effort is part of the third phase of a broad-scoped and systematic study of sp...
Design and fabrication of sterilization container and model probe assembly for Mars landing capsul
Water cascade heat pump system design and developed for continuous operation in thermal control syst...
High rate multiplexes asymmetry and jitter, data-dependent amplitude variations, and transition dens...
Tests were conducted in the NASA/ARC Unitary Plan wind tunnels on an 0.030-scale replica of the spac...
The comparative program costs associated with use of various standardized spacecraft for Air Force s...
The proximity translation and final docking of the space teleoperator evaluation vehicle (STEV) with...