한국추진공학회:학술대회논문집 (Proceedings of the Korean Society of Propulsion Engineers Conference)
- 한국추진공학회 2011년도 제37회 추계학술대회논문집
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- Pages.144-149
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- 2011
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- 1975-342X(pISSN)
사운딩로켓의 고도 극대화를 위한 최적조건
Optimal Conditions for Maximizing Altitude of Sounding Rocket
- 발행 : 2011.11.24
초록
A study to determine the optimal jet conditions for maximizing altitude of the sounding rocket is conducted. The behavior of a simplified linear momentum equation including aerodynamic drag is investigated. The analytic solutions are obtained and compared with numerical solutions. It is shown that there are the optimal jet conditions for maximizing altitude of a sounding rocket according to the rocket mass ratio.