AIRS in-flight special test results and operational lessons learned
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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This paper will detail some of the key challenges faced while introducing risk management to the mission operations team.
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The International Halley Watch (IHW) was a focused coordination effort to obtain the most complete collection of data ever asembled on a comet.
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The Mission Execution and Automation Section, Information Technologies and Software Systems Division at the Jet Propulsion Laboratory, recently delivered an animated software training module for the TMOD UPLINK Consolidation Task for operator training at the Deep Space Network.
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The evolution of a linear servoactuator design is presented. The linear actuator was needed to position Cassini's redundant rocket motors. A device design inherited from JPL's Mariner and Viking Mars missions served as a starting point. The various improvements made and the efforts involved in developing new component sources are discussed. Because the brush type DC motor from the old design was retained, special attention was placed on the reliability testing of the motor and mechanism at all stages of procurement and assembly.
The TDRSS Space VLBI demonstrations performed in the late 1980s provided valuable insight into.
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The Supervisory Telerobotics Laboratory (STELER) at the Jet Propulsion Laboratory (JPL) developed a unique local and remote telerobotic system that has been described in earlier articles.
The Cryo System Experiment (CSE), a NASA In-Space Technology Experiments Proram (IN-STEP) Class D Flight Experiment, was developed by Hughes Aircraft Company (Hughes) to validate in zero-g space a 65 K cryogenic system for focal planes, optics, instruments, or other equipment (gramma-ray spectrometers and infrared and submillimeter imaging instruments) that require continuous cryogenic cooling.