Testing of combined air-rocket engine mak-up with pulsing combustion chamber

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Abstract

This paper describes the test results of combined air-rocket engine mak-up at air (V = const) and rocket modes (р = const), the main technical characteristics have been obtained.

About the authors

A. V. Solodovnikov

Serpukhov military institution of missile forces

Author for correspondence.
Email: aleksey.solod@mail.ru

the chair teacher

Russian Federation

E. N. Vishegorodcev

Serpukhov military institution of missile forces

Email: varvsn@mail.ru

candidate of engineering sciences
chair chief

Russian Federation

V. V. Golubyatnik

Serpukhov military institution of missile forces

Email: slava6123@rambler.ru

candidate of engineering sciences

Russian Federation

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