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Experimental research of staff LTRE with hypergolic propellant under impulse engaging conditions
- Authors: Shustov S.A.1
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolev (National Research University)
- Issue: Vol 10, No 3-4 (2011): Special Issue
- Pages: 273-278
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/7007
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-4(27)-273-278
- ID: 7007
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Abstract
The results of the experimental research of dynamic characteristics of staff LTRE with thrust from 10 N to 130 N with hypergolic propellant under impulse engaging conditions are described. The formation specific of front and behind impulse connected with explosive character of working procedure during 1 ms is defined. The influence of the LTRE volume upon the basic dynamic parameters is analyzed.
About the authors
S. A. Shustov
Samara State Aerospace University named after academician S.P. Korolev (National Research University)
Author for correspondence.
Email: shustov.st@yandex.ru
Candidate of Technical Sciences, Associate Professor
Russian FederationReferences
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