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An effective design method for a pyrotechnic separation device is presented using a developed mathematical model. The optimization resulted in about 4.5 times improved performance index with respect to the reference model.
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This page is a summary of: Performance Optimization of a Split-Type Low-Shock Separation Bolt, Journal of Spacecraft and Rockets, September 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34783.
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