Autor:	J. W. Hadley
Rok vydání:	1963
Předmět:	Engineering Temperature control business.product_category Rocket Mathematical model business.industry Aerospace engineering Propulsion Pressure dependence business Pressure vessel Pulse (physics)
DOI:	10.2172/456297
Popis:	This note derives some relationships between the various parameters describing the nuclear pulse rocket, and gives numerical examples of performance attainable under the assumption of a fixed chamber temperature.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::289dcfcc38bb63ca7480f380823d05e5 https://doi.org/10.2172/456297 Zobrazit plný text záznamu