Solution of the problems of spacecraft aerothermodynamics

Authors:
  • YDYa. A. Dem’YAnov
    Ya. A. Dem’YAnov
  • VLV. I. Lapygin
    V. I. Lapygin
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Abstract
The review presents the materials concerning investigation of aerogasdynamics and thermal protection of missiles during their launch and flight and of re-entering spacecraft accomplished from the foundation of NII-88 (now TsNIIMash) to Gagarin’s flight. The experimental and theoretico-computational studies, chiefly not reported in accessible publications, are outlined.