Firing test stand pulse detonation low-thrust engines
- Authors: Govorenkho G.S.1, Teterin D.P.1, Kotelnikhov D.S.1, Aliluev A.V.1, Aliluev S.V.1, Fedorets V.N.1
-
Affiliations:
- «Electropribor» Design Bureau, Saratov
- Issue: Vol 8, No 3-1 (2009): Special Issue
- Pages: 97-105
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/681
- DOI: https://doi.org/10.18287/2541-7533-2009-0-3-1(19)-97-105
- ID: 681
Cite item
Full Text
Abstract
In the article experience of creation a test stand of pulse detonation engines is stated. Stand operating modes, representation and information machining, order of conducting fire tests are presented structure and functions of the test stand, possibility used technical and software.
About the authors
G. S. Govorenkho
«Electropribor» Design Bureau, Saratov
Author for correspondence.
Email: vest@ssau.ru
Russian Federation
D. P. Teterin
«Electropribor» Design Bureau, Saratov
Email: vest@ssau.ru
Russian Federation
D. S. Kotelnikhov
«Electropribor» Design Bureau, Saratov
Email: vest@ssau.ru
Russian Federation
A. V. Aliluev
«Electropribor» Design Bureau, Saratov
Email: vest@ssau.ru
Russian Federation
S. V. Aliluev
«Electropribor» Design Bureau, Saratov
Email: vest@ssau.ru
Russian Federation
V. N. Fedorets
«Electropribor» Design Bureau, Saratov
Email: vest@ssau.ru
Russian Federation