Effect of RP-1 Compositional Variability on Thermal Conductivity at High Temperatures and High Pressures

Autor:	Ilmutdin M. Abdulagatov, Lala A. Akhmedova-Azizova, Thomas J. Bruno
Rok vydání:	2009
Předmět:	business.product_category Steady state Chemistry General Chemical Engineering Thermal decomposition Energy Engineering and Power Technology Thermodynamics Rocket propellant Atmospheric temperature range Fuel Technology Thermal conductivity Rocket High pressure Fusee business
Zdroj:	Energy & Fuels. 23:4522-4528
ISSN:	1520-5029 0887-0624
DOI:	10.1021/ef900435b
Popis:	The thermal conductivity of rocket propellant RP-1 has been measured with a coaxial-cylinder (steady-state) technique. Measurements were made in the temperature range from 292 to 732 K and at press...
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::227529b42960c9344b8e3881fff1a04b https://doi.org/10.1021/ef900435b Zobrazit plný text záznamu