Email this article 
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
- Authors: Silyutin M.V.1, Shustov S.A.1
-
Affiliations:
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 205-212
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6881
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-205-212
- ID: 6881
Cite item
Full Text
Abstract
Based on the experimental study a suggested physical model working processes in the combustion chamber LREST with jet-centrifugal jets on the hypergolic propellants into six interrelated areas.
About the authors
M. V. Silyutin
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Author for correspondence.
Email: tdla@ssau.ru
assistant
Russian FederationS. A. Shustov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: tdla@ssau.ru
Candidate of technical Sciences
associate Professor
References
Supplementary files
