The Mariner Jupiter/Saturn infrared instrumentation conceptual design study was conducted to determine the physical and operational characteristics of the instruments needed to satisfy the experiment science requirements. The design of the instruments is based on using as many proven concepts as possible. Many design features are taken from current developments such as the Mariner, Pioneer 10, Viking Orbiter radiometers, and Nimbus D spectrometer. Calibration techniques and error analysis for the instrument system are discussed
Three ozone tape products from the Solar Backscatter Ultraviolet (SBUV) experiment aboard Nimbus 7 w...
Optimizing propulsion systems and trajectories of interplanetary spacecraft - numerical analyses and...
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...
A brown dwarf star having only 20-50 times the mass of Jupiter is located below and to the left of t...
The second task of a study with the overall objective of providing a conceptual definition of the Te...
Remote-controlled man-machine system for space exploration analyzed in Mars spacecraft system stud
Stability and control, telecommunication system, solar array design, propellant feed system, and inf...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
The laser atmospheric wind sounder (LAWS) will provide a new space based capability for the direct m...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
Instrumentation for chemical analysis of planetary environment and extraterrestrial lif
Attitude control is reviewed, encompassing the attitude control subsystem, spacecraft attitude preci...
Voyager spacecraft sterilization - launch area operations, biological barrier, microbiological analy...
The NASA Manned Spacecraft Center has been actively involved in the direction and support of program...
A detailed system level design of an Optical Transceiver Package (OPTRANSPAC) for a deep space vehic...
Three ozone tape products from the Solar Backscatter Ultraviolet (SBUV) experiment aboard Nimbus 7 w...
Optimizing propulsion systems and trajectories of interplanetary spacecraft - numerical analyses and...
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...
A brown dwarf star having only 20-50 times the mass of Jupiter is located below and to the left of t...
The second task of a study with the overall objective of providing a conceptual definition of the Te...
Remote-controlled man-machine system for space exploration analyzed in Mars spacecraft system stud
Stability and control, telecommunication system, solar array design, propellant feed system, and inf...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
The laser atmospheric wind sounder (LAWS) will provide a new space based capability for the direct m...
The feasibility of dividing the 8-12 micrometer thermal infrared wavelength region into six spectral...
Instrumentation for chemical analysis of planetary environment and extraterrestrial lif
Attitude control is reviewed, encompassing the attitude control subsystem, spacecraft attitude preci...
Voyager spacecraft sterilization - launch area operations, biological barrier, microbiological analy...
The NASA Manned Spacecraft Center has been actively involved in the direction and support of program...
A detailed system level design of an Optical Transceiver Package (OPTRANSPAC) for a deep space vehic...
Three ozone tape products from the Solar Backscatter Ultraviolet (SBUV) experiment aboard Nimbus 7 w...
Optimizing propulsion systems and trajectories of interplanetary spacecraft - numerical analyses and...
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...