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Cubesat Minimoon Re...
Cubesat Minimoon Rendezvous Mission Synthesis and Analysis
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- Anthony, Niklas (författare)
- Luleå tekniska universitet,Rymdteknik
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- Emami, M. Reza (författare)
- University of Toronto, Canada
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(creator_code:org_t)
- International Astronautical Federation, 2018
- 2018
- Engelska.
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Ingår i: IAC-18. - : International Astronautical Federation.
- Relaterad länk:
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https://urn.kb.se/re...
Abstract
Ämnesord
Stäng
- This paper introduces a mission concept for the remote characterization of a temporarily-captured asteroid, or “minimoon”, based on the utilization of the CubeSat form-factor. Minimoons are a subpopulation of the estimated two million Near-Earth Objects (NEOs) under 2 meters in diameter, which pass within the Moon’s orbit every year. These temporarily-captured objects do not remain in the Earth-Moon system for long, typically less than one year, and are thus a challenge for developing conventional spacecraft missions. A potential solution to this problem is to utilize the typical rapid-development timelines that CubeSat missions possess. This paper will analyze the requirements and limitations in developing a mission for a CubeSat to rendezvous or fly by a minimoon. This includes exploring the capabilities and applicability of the CubeSat technologies for such a mission, analyzing the erratic nature of minimoon orbits, lying out how such a mission project would be managed, and finally presenting a case study of such missions on the only known minimoon so far, Asteroid 2006 RH120.
Ämnesord
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)
Nyckelord
- Onboard space systems
- Rymdtekniska system
Publikations- och innehållstyp
- ref (ämneskategori)
- kon (ämneskategori)