Determination of the Flow Field in the Propellant Tank of a Rocket Engine on Completion of the Mission

Author:

Fedorov A. V.,Bedarev I. A.,Lavruk S. A.,Trushlyakov V. I.,Kudentsov V. Yu.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,Condensed Matter Physics

Reference10 articles.

1. A. V. Fedorov and V. M. Fomin, Mathematical simulation of the behavior of a population of artificial satellites in nearearth space, Fiz. Goreniya Vzryva, No. 5, 142−148 (1994).

2. Ya. T. Shatrov, Ensuring Environmental Safety of Aerospace Activity: a Textbook [in Russian], TsNIIMASh, Korolev (2010).

3. R. P. Patera, K. R. Bohman, and M. A. Landa, Controlled deorbit of the DELTA IV upper stage for the DMSP-17 mission, in: Proc. 2nd IAASS Conf. "Space Safety in a Global World," 14−16 May 2007, Chicago, USA (ESA SP-645, July 2007).

4. Kazuo Takase, Masanori Tsuboi, Shigeru Mori, and Kiyoshi Kobayashi, Successful demonstration for upper stage controlled re-entry experiment by H-IIB launch vehicle, Mitsubishi Heavy Industries Technical Review, 48, No. 4, 11–16 (2011).

5. V. Yu. Kudentsov, V. I. Trushlyakov, and V. V. Shalai, Development of an active vehicle-mounted deorbiting system, Kosmonavtika Raketostroenie, 57, No. 4, 122–128 (2009).

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