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

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

Russian Federation

the chair teacher

E. N. Vishegorodcev

Serpukhov military institution of missile forces

Email: varvsn@mail.ru

Russian Federation

candidate of engineering sciences
chair chief

V. V. Golubyatnik

Serpukhov military institution of missile forces

Email: slava6123@rambler.ru

Russian Federation

candidate of engineering sciences

References

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