Study of Spacecraft Deployables Failures
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Spacecraft Deployables↗
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Results for “deployables”
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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A Deployable 40 kWe Lunar Fission Surface Power Concept
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FSP↗
Meteorological Overview of the 2021 and 2022 DCTOSS Deployment
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Meteorological↗
International Space Station Satellite Deployment: Jettison Policy and Best Practices for Satellite Payload Developers
The International Space Station Systems Engineering and Integration Office is responsible for the Multilateral International Space Station (ISS) and ISS Visiting Vehicle Jettison Policy, the Partner Program Directive on jettisoning objects from the ISS and Visiting Vehicles to/from the ISS.
Jettison Policy↗
Design of Shape-Adaptive Deployable Slat-Cove Filler for Airframe Noise Reduction
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Gaetano Arena↗
Parachute deployment on Venus : Recovery of “Lost” Pioneer Venus large probe entry accelerometer data
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Ralph D. Lorenz↗
Deploying temporary networks for upscaling of sparse network stations
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Evan J. Coopersmith↗
Development of a Multispectral Albedometer and Deployment on an Unmanned Aircraft for Evaluating Satellite Retrieved Surface Reflectance over Nevada’s Black Rock Desert
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Jayne M. Boehmler↗
Forward dynamics analysis of origami-folded deployable spacecraft structures
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JoAnna Fulton↗
Cadmium-sulfide solar cells in a deployable array composed of rigid frames.
Si and Cd solar cell arrays compared using rigid frame Si solar cell concept
SOLAR CELL↗
Structural problems associated with development of large, deployable, solar-cell arrays.
Structural problems in high power solar photovoltaic arrays technology, discussing configuration, materials selection, thermal control coatings and tests results
MATERIAL TESTING↗
Positive deployable solar array development program Final report, 1 Jul. - 30 Sep. 1964
Design criteria for compact, storable solar array for use with spin stabilized satellites
Source record↗
Flight test of a 40-foot-nominal-diameter modified ringsail parachute deployed at a Mach number of 1.64 and a dynamic pressure of 9.1 pounds per square foot
Flight tests of ringsail parachute with 15 percent porosity, for planetary entry
Eckstrom, C. V.↗
Flight test of a 30 foot nominal diameter cross parachute deployed at a Mach number of 1.57 and a dynamic pressure of 9.7 pounds per square foot
Flight test of 30 foot nominal diameter cross parachute to measure shock loads, drag efficiency, and stability characteristics
Eckstrom, C. V.↗
Relative rating of 9' - 16' deployed diameter spaceborne antenna erecting techniques.
Spaceborne paraboloidal antennas erecting techniques, considering applicability to near earth or interplanetary missions
Radany, E. W.↗
Full-scale simulation of parachute deployment environment in the atmosphere of Mars.
Flight test program to investigate operating characteristics of large size parachutes in environment simulating Mars atmosphere
Bendura, R. J.↗
Low-speed deployment, inflation, and steady- descent characteristics of ram-air-inflated balloon recovery systems with peripheral airscoop
Free flight performance characteristics of ram air inflated recovery balloons with peripheral airscoops
Burk, S. M., Jr.↗
Flight test of a 40 foot nominal diameter disk-gap-band parachute deployed at a Mach number of 3.31 and a dynamic pressure of 10.6 pounds per square foot
Performance test on disk gap band parachute at supersonic speeds
Eckstrom, C. V.↗