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Design and In-Orbit Performance of the Heat Shield Insulation for Liquid Apogee Motor of INSAT-2A and INSAT-2B
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English
Abstract
A super insulated (multi layer insulation) heat shield has been designed and implemented for the 440 N Liquid Apogee Motor (LAM) of INSAT-2A and INSAT-2B satellites. The design had been arrived at its final configuration after a series of test and detailed analysis of the test data. An effective conductivity and emissivity for the shield insulation assembly was estimated and used for predicting the flight performance.
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Citation
Bhide, R. and Kaila, V., "Design and In-Orbit Performance of the Heat Shield Insulation for Liquid Apogee Motor of INSAT-2A and INSAT-2B," SAE Technical Paper 941585, 1994, https://doi.org/10.4271/941585.Also In
References
- INSAT-1 Space Segment Project Preliminary Design Review January 1979
- Critical Design Review Thermal July 1979
- INSAT-1A Spacecraft Performance Evaluation by INSAT-1 SSPO April 1982
- INSAT-2B Spacecraft Performance Evaluation by INSAT-1 SSPO October 1983
- INSAT-2C Spacecraft Performance Evaluation Report by INSAT-1 SSPO September 1988
- INSAT-1D Spacecraft Sub-system Performance
- Thermal Analysis Of Test On LAM Heat Shield Conducted at HATF Mahendragiri April 1990
- Design And Analysis Of Thermal System of INSAT-II TS December 1990
- INSAT-2 Spacecraft Critical Design Review Of Thermal Critical System December 1990