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Definition of Engine Component Performance Test Range of 75tf Class Gas Generator Cycle Liquid Propellant Rocket Engine  

Nam, Chang-Ho (한국항공우주연구원 발사체 엔진팀)
Moon, Yoon-Wan (한국항공우주연구원 발사체 엔진팀)
Seol, Woo-Seok (한국항공우주연구원 발사체 엔진팀)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.15, no.6, 2011 , pp. 91-97 More about this Journal
Abstract
A test range for a 75tf class gas generator cycle liquid propellant rocket engine is defined. The engine system test range is defined by the performance variation during flight, the dispersion after engine calibration, and additional margin. The component development test range includes the operation range corresponding to the engine system test range and the component performance margin.
Keywords
Liquid Propellant Rocket Engine; Component; Test; Range;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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