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Development of thermal energy storage units for spacecraft cryogenic coolersThermal Energy Storage Units were developed for storing thermal energy required for operating Vuilleumier cryogenic space coolers. In the course of the development work the thermal characteristics of thermal energy storage material was investigated. By three distinctly different methods it was established that ternary salts did not release fusion energy as determined by ideality at the melting point of the eutectic salt. Phase change energy was released over a relatively wide range of temperature with a large change in volume. This strongly affects the amount of thermal energy that is available to the Vuilleumier cryogenic cooler at its operating temperature range and the amount of thermal energy that can be stored and released during a single storage cycle.
Document ID
19800034194
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richter, R.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Mahefkey, E. T.
(USAF, Aero Propulsion Laboratory, Wright-Patterson AFB Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 80-0145
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A18364
Funding Number(s)
CONTRACT_GRANT: F33616-75-C-2045
Distribution Limits
Public
Copyright
Other

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