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The development of structural elements of missiles, which are separated during flight and burn up in the atmosphere, is proposed. For this, pyrotechnic compositions are introduced into the structure material.
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This page is a summary of: Methodology for the Design of Combustible Structures of Separating Launch Vehicle Parts, Journal of Spacecraft and Rockets, March 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34920.
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