Prometheus Asteroid Redirection Mission : Mission Design, Spacecraft Design, Orbital Dynamics Code Development
This report will design a mission and spacecraft to redirect the first Near-Earth Object (NEO) to a stable orbit in the Earth-Moon system. The mission profile includes a soon-as-possible launch, spiral-out escape from the Earth-Moon system, rendezvous, ion beam redirection method, and decommissionin...
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| Format: | Others |
| Language: | English |
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Luleå tekniska universitet, Institutionen för system- och rymdteknik
2016
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-174 |