Proceedings of the Korean Society of Propulsion Engineers Conference (한국추진공학회:학술대회논문집)
- 2012.05a
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- Pages.451-453
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- 2012
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- 1975-342X(pISSN)
Conceptual Design and Manufacturing Scheme of a Gas Generator for 7 tonf Class Rocket Engine
7톤급 로켓엔진 가스발생기 개념설계 및 제작계획
- Published : 2012.05.17
Abstract
Conceptual design and manufacturing scheme of a gas generator for 7 tonf class rocket engine were described. The combustion chamber pressure, O/F ratio, and total flow rate were decided to be 6 MPa, 0.321, and 1 kg/s respectively in consequence of the engine system design. Based on the parameters conceptual design of the gas generator was carried out and its outer dimension was about
7톤급 로켓엔진 가스발생기에 대한 개념설계와 제작방법에 대해서 기술하였다. 엔진 시스템 설계의 결과로서 연소실 압력, 혼합비, 전체유량이 각각 6 MPa, 0.321, 1kg/s로 결정되었다. 이 변수들을 기본으로 가스발생기의 개념설계가 수행되었고 외형 치수는 대략
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