Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2009.11a
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- Pages.181-184
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- 2009
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- 1975-342X(pISSN)
A Formulation and Performance Characteristics of Composite Solid Propellant for an Application to Gas Generators
기체발생기용 복합고체추진제의 조성 및 성능특성 연구
Abstract
A development of a composite solid propellant is carried out for an application to gas generators as an energy source of rocket system. With HTPB as a propellant binder which has 80% of particle loading ratio, a favorable rheology, and moderate curing properties at the range of
로켓시스템의 에너지원으로 적용할 수 있는 기체발생기용 복합 고체추진제의 개발과정을 기술한다. 80%의 고체입자 부하율과 양호한 유동성, 그리고
Keywords