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This article is cited in 10 scientific papers (total in 10 papers)
Urgent communication
Estimating the mass of a pyrotechnic mixture for burning the launch vehicle nose fairing
D. B. Lemperta, V. I. Trushlyakovb, V. E. Zarkocd a Institute of Problems of Chemical Physics, Russian Academy of Sciences, Chernogolovka, 142432, Russia
b Omsk State Technical University, Omsk, 644050, Russia
c Voevodsky Institute of Chemical Kinetics and Combustion, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia
d Tomsk State University, Tomsk, 634050, Russia
Abstract:
It is proposed to carry out burning of the launch vehicle nose fairing after it has completed its mission on the descent trajectory from the moment of separation to an altitude of 5–10 km. Burning is carried out in the Earth atmosphere with additional heating of the faring material due to the reaction of pyrotechnic mixtures. Various pyrotechnic mixtures for use in the nose fairing are discussed.
Keywords:
burning, fairing, launch vehicle, pyrotechnic mixture.
Received: 10.02.2015 Revised: 06.04.2015
Citation:
D. B. Lempert, V. I. Trushlyakov, V. E. Zarko, “Estimating the mass of a pyrotechnic mixture for burning the launch vehicle nose fairing”, Fizika Goreniya i Vzryva, 51:5 (2015), 121–125; Combustion, Explosion and Shock Waves, 51:5 (2015), 619–622
Linking options:
https://www.mathnet.ru/eng/fgv267 https://www.mathnet.ru/eng/fgv/v51/i5/p121
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