한국전산유체공학회:학술대회논문집
- 2008.03b
- /
- Pages.707-710
- /
- 2008
Develop Test Facility of High Altitude Environment for Kick Motor
Kick Motor용 고공환경 모사 시험 설비 개발
-
Kim, Sang-Heon
;
- V.A, Bershadskiy ;
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Yu, Byung-Il
;
-
Kim, Yong-Wook
;
-
Oh, Seung-Hyub
;
-
Park, Jeong-Joo
- Published : 2008.03.26
Abstract
The method suggested in this thesis is the safe and economic method when testing rocket engine because ground test facility copies high altitude. We have decided to use the schematic of testing facility based on already known design method and test result, and we have decided the test condition for ground firing test of solid fuel. In addition the pressure of nozzle exit area is 0.1bar, we have designed the testing facility structure to test in this condition. Moreover, we have designed to reduce the accident probability.