Measurements of specific impulse of solid rocket propellants

Measurements of specific impulse of solid rocket propellants

Bibliographic Details
Parent link:Advances in Nonequilibrium Processes: Plasma, Combustion, and Atmosphere/ [eds. A. M. Starik, S. M. Frolov]. P. 179-183.— , 2014
Corporate Author: Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра атомных и тепловых электростанций (АТЭС)
Other Authors: Korotkikh A. G. Aleksandr Gennadievich, Arkhipov V., Kiskin A., Zarko V., Yankovsky S. A. Stanislav Aleksandrovich
Summary: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
Language:Russian
Published: 2014
Series:Part three: Combustion
Subjects:
труды учёных ТПУ
удельный импульс
твердое ракетное топливо
продукты газификации
поверхность горения
Format: Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=602303

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