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Combustion Explosion and Shock Waves
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Estimating the mass of a pyrotechnic mixture for burning the launch vehicle nose fairing

descriptionPublicationkeyboard_double_arrow_right Article 01 Sep 2015 English Publisher:Pleiades Publishing LtdJournal:Combustion, Explosion, and Shock Waves, volume 51, pages 619-622 (issn: 0010-5082, eissn: 1573-8345, Copyright policy )
Authors: Vladimir E. Zarko; Vladimir E. Zarko; V. I. Trushlyakov; D. B. Lempert;

doi: 10.1134/s0010508215050147

Estimating the mass of a pyrotechnic mixture for burning the launch vehicle nose fairing

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.

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Keywords

обтекатели, пиротехнические смеси, горение, ракеты-носители

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
9
Average
Top 10%
Average
Green
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