TEST INSTALLATION FOR SMALL-SIZE SPACE PROPULSION SYSTEMS

The invention relates to a test installation for small-size space propulsion systems, with traction developed in the range of 0.1...20 N, designed to control the attitude and change of the space platform orbit and operating under conditions of sub-atmospheric pressure. The test installation for smal...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VILAG VALERIU ALEXANDRU, NICOARĂ RĂZVAN EDMOND, VILAG JENI ALINA, PRISĂCARIU EMILIA GEORGIANA, MACRIŞOIU NICOLAE
Format: Patent
Sprache:eng ; rum
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