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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국우주과학회 Journal of Astronomy and Space Sciences Journal of Astronomy and Space Sciences 제32권 제3호
- 발행연도
- 2015.9
- 수록면
- 257 - 268 (12page)
- DOI
- http://dx.doi.org/10.5140/JASS.2015.32.3.257
이용수
초록· 키워드
오류제보하기
Characteristics of delta-V requirements for deploying an impactor from a mother-ship at different orbital altitudes are analyzed in order to prepare for a future lunar CubeSat impactor mission. A mother-ship is assumed to be orbiting the moon with a circular orbit at a 90 deg inclination and having 50, 100, 150, 200 km altitudes. Critical design parameters that are directly related to the success of the impactor mission are also analyzed including deploy directions, CubeSat flight time, impact velocity, and associated impact angles. Based on derived delta-V requirements, required thruster burn time and fuel mass are analyzed by adapting four different miniaturized commercial onboard thrusters currently developed for CubeSat applications. As a result, CubeSat impact trajectories as well as thruster burn characteristics deployed at different orbital altitudes are found to satisfy the mission objectives. It is concluded that thrust burn time should considered as the more critical design parameter than the required fuel mass when deducing the onboard propulsion system requirements.
Results provided through this work will be helpful in further detailed system definition and design activities for future lunar missions with a CubeSat-based payload.
목차
등록된 정보가 없습니다.
참고문헌 (26)
참고문헌 신청
Blaney DL / 2012 / Interplanetary CubeSats: Small, low cost missions beyond low Earth Orbit / Proceedings of the 43rd Lunar and Planetary Science Conference
Brent, RP / 2002 / Algorithms for minimization without derivatives / Dover publication :18~79
BUSEK / Green Monopropellant Thrusters
Curtis HD / 2009 / Orbital Mechanics for Engineering Students / Elsevier :61~69
엄위섭 / 2012 / Study on a Suspension of a Planetary Exploration Rover to Improve Driving Performance During Overcoming Obstacles / Journal of Astronomy and Space Sciences 29(4):381~387
Brent, RP / 2002 / Algorithms for minimization without derivatives / Dover publication :18~79
BUSEK / Green Monopropellant Thrusters
Curtis HD / 2009 / Orbital Mechanics for Engineering Students / Elsevier :61~69
엄위섭 / 2012 / Study on a Suspension of a Planetary Exploration Rover to Improve Driving Performance During Overcoming Obstacles / Journal of Astronomy and Space Sciences 29(4):381~387
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