Modeling the Process of Vapor–Gas Mixture Outflow from the Drainage Manifold of the Rocket-Carrier Stage

Author:

Zharikov K. I.,Trushlyakov V. I.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,Condensed Matter Physics

Reference27 articles.

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2. V. V. Biryuk, V. A. Kapitonov, and A. V. Smorodin, Increase of the efficiency of supercharging systems of fuel tanks of rocket-carriers in the process of flight, Vestn. Saratovsk. Gos. Agr. Univ., No. 3. pp. 21–26 (2008).

3. G. F. R. Duarte, Aerodynamic heating of missile/rocket — conceptual design phase, in: Proc. 20th Int. Cong. of Mech. Eng., November 15–20, 2009, Gramado, RS, Brazil (2009).

4. V. I. Trushlyakov and K. I. Zharikov, Simulating heat load of a cryogenic fuel tank of a spent launcher orbiter to evaluate explosive rupture, Indian J. Sci.Technol., 9, No. 36, 102036 (2016).

5. N. L. Johnson, E. Stansbery, D. O. Whitlock, K. J. Abercromby, and D. Shoots, History of On-Orbit Satellite Fragmentations, 14th edn., Houston, Texas: NASA Johnson Space Center, (2008).

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