The hardware challenges for the Mars Exploration Rover Heat Rejection System
UNKNOWN
mechanically-pump↗
Engineering topics
Tsuyuki, G.
Publications and source records attributed to Tsuyuki, G..
JPL's thermal testing philosophy
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thermal test↗
Mars Exploration Rover: Thermal design is a system engineering activity
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thermal design system engineering lessons learned↗
Reflight of the Mars Pathfinder integrated pump assembly for the Mars Exploration Rover 2003 project
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mechanical pump Mars↗
Thermal balance test verification of the Galaxy Evolution Explorer (GALEX) thermal design
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GALEX Galaxy Evolution Explorer thermal design↗
Use of Passive Versus Active Systems
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thermal control active passive↗
Novel Lightweight Thermal Insulation Types for the Martian Environment: Using Carbon Dioxide Gas and Aerogel in Lightweight Enclosures
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thermal insulation aerogel insulation lightweight ↗
Integrating Thermal Tools Into the Mechanical Design Process
The intent of mechanical design is to deliver a hardware product that meets or exceeds customer expectations, while reducing cycle time and cost.
mechanical↗
A Summary of the Cassini Spacecraft Thermal Performance from Launch Through Early Cruise
Cassini, NASA's mission to investigate the Saturnian system was launched successfully on October 15, 1997.
Cassini↗
A Summary of the Cassini Spacecraft Thermal Performance from Launch through Early Cruise
Cassini, NASA's mission to investigate the Saturnian system was launched successfully on October 15, 1997.
Cassini↗
Keeping Warm on Mars: Strategies for Micromission Thermal Design
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native resources Mars convective losses radiative ↗
On-Orbit Thermal Performance of A Submillimeter Telescope Primary Reflector Panel
An Optimized thermal design for the SMILS Telescope has been developed. This design has demonstrated that the expected on-orbit lateral temperature gradient in the primary reflector has been minimized.
Thermal↗
On-Orbit Thermal Performance of a Submillimeter Telescope Primary Reflector Panel
A detailed thermal analysis has been performed for a panel of a segmented primary mirror which is closest to the high side of the telescope sunshade. This panel was selected because the spatial temperature distribution was expected to be the worst. The JPL90-10 primary reflector panel configuration was investigated because of its superior figure error performance in ground-based testing.
SMILS↗
Spatial and temporal temperature distribution optimization for a geostationary antenna
The Geostationary Microwave Precipitation Radiometer antenna is considered and a thermal design analysis is performed to determine a design that would minimize on-orbit antenna temporal and spatial temperature gradients. The final design is based on an optically opaque radome which covered the antenna. The average orbital antenna temperature is found to be 9 C with maximum temporal and spatial variations of 34 C and 1 C, respectively. An independent thermal distortion analysis showed that this temporal variation would give an antenna figure error of 14 microns.
Tsuyuki, G.↗