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- Article name
- Working out of manufacturing of carbon-ceramic combustion chamber of liquid rocket engine with low thrust
- Authors
- RAZINA A. S., , as.razina@gmail.com, University of Technology; JSC "Kompozit", Korolev, Moscow region, Russia
SERDYUK E. A., , rayman47@mail.ru, University of Technology; JSC "Kompozit", Korolev, Moscow region, Russia
BOGACHEV E. A., , eug-bogatchev@mail.ru, University of Technology; JSC "Kompozit", Korolev, Moscow region, Russia
IZOTOV V. D., , 9015460113@list.ru, JSC "Kompozit", Korolev, Moscow region, Russia
- Keywords
- combustion chamber / liquid rocket engine / low thrust / carbon-carbon composite material / carbon-ceramic composite material / direct molding / tooling
- Year
- 2017 Issue 1 Pages 34 - 37
- Code EDN
- Code DOI
- Abstract
- It was noted that the further development of orbital and space technology requires materials with significantly improved properties. A large specific gravity, poor oxidation and corrosion resistance at high temperatures (above 1100 °C), limit the use of available materials for the manufacture of articles such as rocket engine combustion chamber intended for systems of orbital and shunting of spacecraft. Presents results working out of the combustion chamber of the rocket engine low thrust manufacturing process of carbon-ceramic composite material.
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