A variable-thrust solid-propellant rocket engine with local combustion boosting-Reference-Cited by-同舟云学术

A variable-thrust solid-propellant rocket engine with local combustion boosting

Published:1996-05 Issue:3 Volume:32 Page:327-330
ISSN:0010-5082
Container-title:Combustion, Explosion, and Shock Waves
language:en
Short-container-title:Combust Explos Shock Waves

Author:

Petrenko V. I.,Popov V. L.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Link

http://link.springer.com/content/pdf/10.1007/BF01998464.pdf

Reference8 articles.

1. V. M. Bobylev,Solid-Propellant Rocket Engine as a Means of Rocket Motion Control [in Russian], Mashinostroenie, Moscow (1992).

2. V. I. Petrenko, V. L. Popov, A. M. Rusak, and V. I. Feofilaktov,Variable-Thrust SPRE [in Russian], Press of State Rocket Center “Academician V. P. Makeev KB,” Miass (1994).

3. A. D. MacDonald, “A multiple-start variable-thrust SPRE,”Vopr. Raket. Tekh., No. 2, 32–50 (1973).

4. A. M. Rusak, “Steady-state characteristics of gas producers with a variable combustion area,”Izv. Vyssh. Uchebn. Zaved., Aviats. Tekh., No. 4, 73–77 (1988).

5. W. Buschulte, “Zur Schubregelung von Feststoffraketen — betribwerken,” Zeitschrift fur Flugwissenschaften und Weltraumforschung,1, No. 5, 358–364 (1977).

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