Measurements of specific impulse of solid rocket propellants; Advances in Nonequilibrium Processes: Plasma, Combustion, and Atmosphere

Xehetasun bibliografikoak
Parent link:Advances in Nonequilibrium Processes: Plasma, Combustion, and Atmosphere.— 2014.— P. 179-183
Erakunde egilea: Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра атомных и тепловых электростанций (АТЭС)
Beste egile batzuk: Korotkikh A. G. Aleksandr Gennadievich, Arkhipov V., Kiskin A., Zarko V., Yankovsky S. A. Stanislav Aleksandrovich
Gaia:A new laboratory technique is presented for fast determination of the specific impulse of solid rocket propellants (SRPs), based on the measurement of recoil force of gasification products flowing from the burning surface of solid propellants. The values of specific impulse for the model composite solid propellant are obtained while varying the pressure in the combustion chamber.
В фонде НТБ ТПУ отсутствует
Hizkuntza:errusiera
Argitaratua: 2014
Saila:Part three: Combustion
Gaiak:
Formatua: Liburu kapitulua
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=602303

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