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Testing of combined air-rocket engine mak-up with pulsing combustion chamber
- Authors: Solodovnikov A.V.1, Vishegorodcev E.N.1, Golubyatnik V.V.1
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Affiliations:
- Serpukhov military institution of missile forces
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 130-136
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6796
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-130-136
- ID: 6796
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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.
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About the authors
A. V. Solodovnikov
Serpukhov military institution of missile forces
Author for correspondence.
Email: aleksey.solod@mail.ru
the chair teacher
Russian FederationE. N. Vishegorodcev
Serpukhov military institution of missile forces
Email: varvsn@mail.ru
candidate of engineering sciences
chair chief
V. V. Golubyatnik
Serpukhov military institution of missile forces
Email: slava6123@rambler.ru
candidate of engineering sciences
Russian FederationReferences
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