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Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
- Authors: Porshnev V.A.1
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Affiliations:
- JSC «KB Electropribor»
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 200-205
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6807
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-200-205
- ID: 6807
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Abstract
The design procedure of fundamental parameters of the direct-flow detonation pulsing engine (DDPE) for small dimensional the pilotless flying machine is considered. The algorithm of calculation is presented.
About the authors
V. A. Porshnev
JSC «KB Electropribor»
Author for correspondence.
Email: pva@kbep.ru
Candidate of technical Sciences
Head of Sciences Centre
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