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.
Design and In-Orbit Performance of the Heat Shield Insulation for Liquid Apogee Motor of INSAT-2A and INSAT-2B
Sae Technical Papers
International Conference On Environmental Systems ; 1994
1994-06-01
Conference paper
English
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