Ignition transient analysis of a solid rocket motor using a one dimensional two fluid model

Autor:	Byron A. Pardue, Samuel S. Han
Rok vydání:	1992
Předmět:	Ignition system Engineering business.industry law Mechanical engineering Transient response Aerospace engineering Solid-fuel rocket Combustion chamber Transient analysis business Two-fluid model law.invention
Zdroj:	28th Joint Propulsion Conference and Exhibit.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::9ea9cd7cf209a9d286bbb017ab786b89 https://doi.org/10.2514/6.1992-3277 Zobrazit plný text záznamu