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Measurement of Co-efficient of Thermal Expansion of CFRP Strut for IRS-1C Spacecraft ISRO Satellite Centre

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Rāmacāmi, A., author.
Conference Name:
International Conference On Environmental Systems (1994-06-20 : Friedrichshafen, Germany)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1994
Summary:
The measurement of coefficient of thermal expansion of CFRP strut which is planned to be used in Indian Remote Sensing Spacecraft (IRS-1C) has been measured from -10°C to +50°C using an electronic digital indicator. A suitable test rig was designed and fabricated to carry out this measurement in the required temperature range. The coefficient of the thermal expansion results obtained with this testing and technique are accurate to ± 13.4% and the repeatability of this measurement is better than ± 1.3%
Notes:
Vendor supplied data
Publisher Number:
941470
Access Restriction:
Restricted for use by site license

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