METHOD OF COMBINED REMOVAL OF SPACE OBJECT WITH FLAT AERODYNAMIC SAIL FROM NEAR-EARTH ORBIT

The method of combined removal of a space object with a flat aerodynamic sail from a near-Earth orbit involves changing the orientation of the propulsion plant, changing the speed of the space object by a reactive propulsion installation, the formation of an elliptical separation orbit, the deployme...

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Hauptverfasser:	Alpatov Anatolii Petrovych, Dron Mykola Mykhailovych, Lapkhanov Erik Oleksandrovych, Holubek Oleksandr Viacheslavovych
Format:	Patent
Sprache:	eng ; ukr
Online-Zugang:	Volltext bestellen
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