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Flexible radiator system: Executive summaryA full scale prototype flexible radiator panel was designed, built and tested. The panel, has approximately 173 sq ft of radiating area and is designed to reject 1.33 kW of heat to a 0 F sink with a 100 F fluid inlet. The panel is constructed from a flexible Teflon/silver mesh fin surrounding 1/8 inch Teflon tubes. The prototype panel is stowed on a 10 inch diameter by 4 foot wide drum. (It rolls up to a diameter of 17 inches when fully stowed). Deployment of the soft tube prototype is via two four inch diameter Kevlar/Mylar inflation tubes with flat springs incorporated in each tube. Nitrogen is normally used for the deployment with approximately 1 psi required. The springs retract the panels when the inflation tubes are deflated. Another method of deployment available for the soft tube flexible is a motor driven deployable boom. This eliminates the need for expendables when the panel area is varied during the mission for heat load control. The soft tube panel is designed for a 90% probability of no punctured tube in a 30 day mission. The acceptable working fluids for this soft tube flexible are Coolanol 15, Coolanol 20 and Glycol/water (a eutectic mixture).
Document ID
19840012556
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Oren, J. R.
(Vought Corp. Dallas, TX, United States)
Cox, R. L.
(Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
October 30, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
REPT-2-19200/3R-1062B
NASA-CR-171766
NAS 1.26:171766
Report Number: REPT-2-19200/3R-1062B
Report Number: NASA-CR-171766
Report Number: NAS 1.26:171766
Accession Number
84N20624
Funding Number(s)
CONTRACT_GRANT: NAS9-14776
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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