Description of the SERT II spacecraft and mission

Autor:	G. S. Gurski, W. H. Hawersaat, R. G. Goldman
Rok vydání:	1970
Předmět:	Engineering Reliability (semiconductor) Spacecraft Aeronautics Electrically powered spacecraft propulsion Ion thruster business.industry business Spacecraft design
Zdroj:	8th Electric Propulsion Conference.
DOI:	10.2514/6.1970-1124
Popis:	SERT 2 for testing ion thrustor reliability and operational characteristics, discussing design and mission objectives
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::67c8b135128015aa71cd16a34f621d4c https://doi.org/10.2514/6.1970-1124 Zobrazit plný text záznamu