ON THE CYCLIC DEFORMATION OF THE SHELL OF THE COMBUSTION CHAMBER OF A MULTIPLE-ACTION LIQUID-PROPELLANT ROCKET ENGINE

Author:

Zarubin V. S.,Zimin V. N.

Publisher

Allerton Press

Subject

General Physics and Astronomy,Mechanics of Materials

Reference13 articles.

1. V. I. Feodos’ev, Basic Techniques of Rocket Flight (Nauka, Moscow, 1981) [in Russian].

2. V. A. Moiseev, V. A. Tarasov, V. A. Kolmykov, and A. S. Filimonov, Liquid Rocket Engines Production Technology (MGTU Im. Baumana, Moscow, 2008) [in Russian].

3. L. I. Balabukh, K.S. Kolesnikov, V.S. Zarubin, et al., Fundamentals of Structural Mechanics of Rockets (Vysshaya Shkola, Moscow, 1969) [in Russian].

4. N. A. Makhutov, V. S. Rachuk, and M. M. Gadenin, Strength and Resource of Liquid-Fuel Rocket Engines (Nauka, Moscow, 2011) [in Russian].

5. V. S. Zarubin, V. N. Zimin, and G. N. Kuvyrkin, “Estimation of the combustion chamber shell working capacity for the reusable liquid-propellant rocket engine,” Russ. Aeronaut. 61, 425–433 (2018). https://doi.org/10.3103/S1068799818030169

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