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Preliminary tests of tank with cryogenic charging for onboard throttle system of cooling
- Authors: Dovgjallo A.I.1, Sarmin D.V.1, Uglanov D.A.1
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- Issue: Vol 10, No 3-4 (2011): Special Issue
- Pages: 78-84
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6936
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-4(27)-78-84
- ID: 6936
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Abstract
This article deals with first results of tests of a tank with cryogenic charging (liquid nitrogen), which have been made at level of pressure to 4 MPa. Also it is shown that the behavior of parameters in a tank on time corresponds to calculation model.
About the authors
A. I. Dovgjallo
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Author for correspondence.
Email: d.a.i@mail.ru
doctor of technical science, professor
Russian FederationD. V. Sarmin
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: sarmin.d.v@mail.ru
post-graduate student
Russian FederationD. A. Uglanov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: dmitry.uglanov@mail.ru
candidate of technical science
senior lecturer
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