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Development of Tailorable Electrically Conductive Thermal Control Material SystemsThe optical characteristics of surfaces on spacecraft are fundamental parameters in controlling its temperature. Passive thermal control coatings with designed solar absorptance and infrared emittance properties have been developed and have been in use for some time. In this total space environment, the coating must be stable and maintain its desired optical properties as well as mechanical properties for the course of the mission lifetime. The mission lifetimes are increasing and in our quest to save weight, newer substrates are being integrated which limit electrical grounding schemes. All of this has added to already existing concerns about spacecraft charging and related spacecraft failures or operational failures. The concern is even greater for thermal control surfaces that are very large. One way of alleviating such concerns is to design new thermal control material systems (TCMS) that can help to mitigate charging via providing charge leakage paths. The objective of this program was to develop two types of passive electrically conductive TCMS. The first was a highly absorbing/emitting black surface and the second was a low (alpha(sub s)/epsilon(sub N)) type white surface. The surface resistance goals for the black absorber was 10(exp 4) to 10(exp 9) Omega/square, and for the white surfaces it was 10(exp 6) to 10(exp 10) Omega/square. Several material system concepts were suggested and evaluated for space environment stability and electrical performance characterization. Our efforts in designing and evaluating these material systems have resulted in several developments. New concepts, pigments and binders have been developed to provide new engineering quality TCMS. Some of these have already found application on space hardware, some are waiting to be recognized by thermal designers, and some require further detailed studies to become state-of-the-art for future space hardware and space structures. Our studies on baseline state-of-the-art materials and conductive concepts have resulted in several important findings that are of interest to all thermal designers and systems integrators.
Document ID
19980055130
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
Deshpande, M. S.
(IIT Research Inst. Chicago, IL United States)
Harada, Y.
(IIT Research Inst. Chicago, IL United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1997
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA/CR-97-207998
NAS 1.26:207998
Report Number: NASA/CR-97-207998
Report Number: NAS 1.26:207998
Funding Number(s)
CONTRACT_GRANT: NAS8-40580
PROJECT: IITRI Proj. C06804-97
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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