Technologies Developed by and Lessons Learned from the Deep Space 2 Mars Microprobe Project
Explore the source record for details and available documents.
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Explore the source record for details and available documents.
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.
Explore the source record for details and available documents.
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.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
This paper describes scalability issues of evolutionary-driven automatic synthesis of electronic circuits. The article begins by reviewing the concepts of circuit evolution and discussing the limitations of this technique when trying to achieve more complex systems.
Explore the source record for details and available documents.
In this paper, we will summarize the software trends and their impact on the cost of developing flight and ground software.
Explore the source record for details and available documents.
The MicroPrecision Interferometer Testbed (MIP) at JPL is a dynamically and dimensionally representative hardware model of a future spaceborne optical interferometer.
In this paper, the rover navigation performance is analyzed on the basis of received rover telemetry, rover uplink commands and stereo images captured by the lander cameras.
In 1992, Dr. Wes Huntress challenged the JPL staff to undertake the first of NASA's new Discovery Program missions; Pathfinder.
This paper focuses on the onboard planner and scheduler CASPER, whose core planning engine is based on the ground system ASPEN. Given the challenges of developing flight software, we discuss several of the issues encountered in preparing the planner for flight, including reducing the code image size, determining what data to place within the engineering telemetry packet, and performing long term planning.
Explore the source record for details and available documents.
Explore the source record for details and available documents.