Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2008.11a
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- Pages.67-71
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- 2008
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- 1975-342X(pISSN)
Perspectives on the Hot Components for Rocket Nozzle and Thrusters
고성능 로켓노즐 및 추력기용 내열부품 현황
Abstract
Rocket nozzle components and thrusters for next-generation solid rocket with variable thrust, and small uncooled liquid rocket thrusters are required to withstand ultra-high temperature upto
추력조정이 유연한 차세대 고체추진기관 그리고 위성제어용 차세대 비냉각 액체엔진 소형추력기는
Keywords