My Assistant
Cassini-style Trajectory For Neo Tour?, Question about mission feasibility |
Dec 9 2005, 10:39 PM
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Junior Member ![]() ![]() Group: Members Posts: 48 Joined: 8-December 05 Member No.: 603 |
Hi, I’ve been lurking here for a while, but this is my first post. The recent talk on the Uranus & Neptune orbiter forums about Galileo- vs. Cassini-style tours of the moons of the outer planets reminded me of an idea that I had a while ago.
Would it be possible to arrange a Cassini-style trajectory in the Earth-Moon system that would allow periodic visits of NEOs as they passed by? If you limited yourself to visits within 2-3 million km, you would have about one opportunity per year. Lunar gravity assists should provide enough delta-v for the necessary plane changes, and the flyby orbits would have periods of ~100 days, allowing for a few assists between flybys. If you could do close flybys of 5 different NEOs over 5 years without going more than 3 million km from Earth, that would seem like an ideal candidate for a Discovery mission. The potential problem I see with this idea is that Earth’s Hill sphere is only ~1.5 million km, so you’d be spending a good part of each rev orbiting the Sun instead of the Earth. Would it be prohibitive either in terms of time or delta-v to get a spacecraft from a solar orbit 3 million km from Earth to a lunar return trajectory? |
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Dec 12 2005, 02:54 PM
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Solar System Cartographer ![]() ![]() ![]() ![]() Group: Members Posts: 10265 Joined: 5-April 05 From: Canada Member No.: 227 |
I looked into this lunar gravity assist question. The communication satellite was Asiasat 3, named HGS 1 after it was salvaged by Hughes. Its lunar flybys were on 13 May 1998 and 7 June 1998.
I didn't find anything about Genesis doing a lunar flyby to set up its re-entry - it did an Earth flyby, certainly. Possibly it did a lunar flyby initially to get out to L1? That idea of using lunar flybys to get to a Lagrange point was used by WMAP on 30 July 2001. It was done in reverse by ISEE-3 (later renamed ICE, the comet probe) on five occasions, the last on 22 December 1983, to transition from an L1 halo orbit to its comet trajectory. Also, Geotail and Wind, two solar wind probes, used repeated lunar flybys to keep their apogees on the desired side of Earth throughout the year (Geotail on the night side, Wind on the day side). Phil -------------------- ... because the Solar System ain't gonna map itself.
Also to be found posting similar content on https://mastodon.social/@PhilStooke Maps for download (free PDF: https://upload.wikimedia.org/wikipedia/comm...Cartography.pdf NOTE: everything created by me which I post on UMSF is considered to be in the public domain (NOT CC, public domain) |
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Jan 11 2006, 11:53 AM
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![]() Senior Member ![]() ![]() ![]() ![]() Group: Members Posts: 2488 Joined: 17-April 05 From: Glasgow, Scotland, UK Member No.: 239 |
More on the Asiasat 3/HGS 1 Lunar flyby:
http://www.spacedaily.com/news/Book_Reveal...at_In_1997.html Bob Shaw -------------------- Remember: Time Flies like the wind - but Fruit Flies like bananas!
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Bart Cassini-style Trajectory For Neo Tour? Dec 9 2005, 10:39 PM
Bob Shaw Bart:
Earth-Moon slingshots and peculiar orbits s... Dec 9 2005, 11:40 PM
JTN QUOTE (Bob Shaw @ Dec 9 2005, 11:40 PM)About ... Dec 10 2005, 11:22 AM
djellison iirc Genesis used lunar flybys to line up for re-e... Dec 9 2005, 11:43 PM
tasp ICE used several lunar encounters to reach comet G... Dec 10 2005, 03:37 AM![]() ![]() |
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