Add to ORKGDesign, fabrication, installation, and operation of X ray diffractometer and X ray spectrograph system for preliminary examination of lunar soil sample within Lunar Receiving Laborator
The following topics are covered: instrument degradation; the Solar Backscatter Ultraviolet (SBUV) E...
Perovskite oxide materials provide a chemically diverse pseudo cubic ABO3 platform that possesses a ...
The goal of the two phase program is to develop the technology and design and fabricate ultralightwe...
The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Detai...
Communications and television subsystems and radar equipment for Mars 1969, 1971, and 1975 and Venus...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
Laboratory demonstrations that were completed included: (1) an all-solid-state, broadly tunable, sin...
Developing structure, payload, communication and data handling subsystems for ERT
MULTIPAC, multiple pool processor and computer for deep space probe central data syste
Flight test program to obtain data on aided inertial system for terminal guidance and navigation of ...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
A pressurized lunar rover is necessary for future long-term habitation of the moon. The rover must b...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
A proposal was made at the end of 1996 to use the large inventory of RF hardware available after the...
The following topics are covered: instrument degradation; the Solar Backscatter Ultraviolet (SBUV) E...
Perovskite oxide materials provide a chemically diverse pseudo cubic ABO3 platform that possesses a ...
The goal of the two phase program is to develop the technology and design and fabricate ultralightwe...
The three NASA/USAF lunar probes of August 17, October 13, and November 8, 1958 are described. Detai...
Communications and television subsystems and radar equipment for Mars 1969, 1971, and 1975 and Venus...
The development of a laser altimeter for use in the Apollo Lunar Orbital Experiments mission is disc...
Laboratory demonstrations that were completed included: (1) an all-solid-state, broadly tunable, sin...
Developing structure, payload, communication and data handling subsystems for ERT
MULTIPAC, multiple pool processor and computer for deep space probe central data syste
Flight test program to obtain data on aided inertial system for terminal guidance and navigation of ...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
A pressurized lunar rover is necessary for future long-term habitation of the moon. The rover must b...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
The Terminal Configured Vehicle (TCV) program operates a Boeing 737 modified to include a second coc...
A proposal was made at the end of 1996 to use the large inventory of RF hardware available after the...
The following topics are covered: instrument degradation; the Solar Backscatter Ultraviolet (SBUV) E...
Perovskite oxide materials provide a chemically diverse pseudo cubic ABO3 platform that possesses a ...
The goal of the two phase program is to develop the technology and design and fabricate ultralightwe...