Cryogenic Tankage for Chemical Space Power Systems

Autor:	R. J. Corbett, J. M. Lester, J. E. Bell
Rok vydání:	1962
Předmět:	Propellant Electric power system Tank pressure animal structures Nuclear engineering education Mass flow rate Heat leak Environmental science Thrust specific fuel consumption Space exploration Chemical space
Zdroj:	Advances in Cryogenic Engineering ISBN: 9781475705331
DOI:	10.1007/978-1-4757-0531-7_18
Popis:	Various studies have indicated that hydrogen-oxygen propellant systems offer significant advantages over other propellants for short-time space missions. The advantages include weight savings as reflected by an excellent specific fuel consumption and an inherent ability of the cryogenic fluids to absorb large heat inputs.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::45ca18b1122bd741b955df3ac7468ad6 https://doi.org/10.1007/978-1-4757-0531-7_18 Zobrazit plný text záznamu