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Development of low temperature gas generator for filling CMUS inflatable floats

Project Overview

The objective of this project is to develop a solid propellant based low temperature gas generator releasing gases at temperatures less than 120 degree celsius. The sizing will be carried out for filling up a volume of 3 Nos. primary floats of 660 L each and 3 Nos. secondary floats of 400 L at a pressure of 1.2 bar (absolute).

Benefits

The project being undertaken by ISRO in collaboration with academia is directly or indirectly beneficial to the society.
Funding Organization
Quick Information
Thrust Areas
Astronomy & Space Sciences
Focus Area
Propulsion Systems and Space Engineering
Status
Under Development
Source Title
Indian Space Research Organisation (ISRO)- Department of Space (DOS) 2022-2024
Output
Status
Under Development
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