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Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices
- 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: 279-283
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/7008
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-4(27)-279-283
- ID: 7008
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Abstract
The methods and results of experimental research of thermal yet influence of staff LTRE with thrust from 10 N to 100 N with hypergolic propellant under continuous and impulse engaging conditions are expounded. The influence of basic thermo gas and dynamic factors on the thermal influence dimension in the near and far yet part relative to the nozzle cut is described.
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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