SPACECRAFT FOR DESCENT IN ATMOSPHERE OF PLANET AND METHOD OF ITS DESCENT (VARIANTS)

FIELD: rocketry and space engineering; designing descent vehicles at aerodynamic efficiency. SUBSTANCE: proposed spacecraft includes heat-insulated case with blunt nose part, upper and lower parts and bottom protection, as well as landing units. Case is provided with aft control panel which is split...

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Bibliographische Detailangaben
Hauptverfasser: BOLOTIN V.A, MAKAR'EV O.E, DJAD'KIN A.A, BRJUKHANOV N.A, SEMENOV JU.P, RESHETIN A.G
Format: Patent
Sprache:eng
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