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Titan Express?, interesting proposal from Ralph Lorenz |
Aug 25 2009, 10:47 AM
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Senior Member ![]() ![]() ![]() ![]() Group: Members Posts: 3516 Joined: 4-November 05 From: North Wales Member No.: 542 |
With thanks to Van Kane at futureplanets for links to the very interesting white papers for the next decadal survey, here is one that caught my eye:
http://www.google.com/url?sa=t&source=...Wl6DEjXiZwrRDZg Small but capable landers with enough power to talk directly to earth can be hurled into Titan's obliging atmosphere at interplanetary velocities and land safely without parachutes. QUOTE: Mission Architecture A network mission could likely (depending on the ASRG/RTG provision) fit within the New Frontiers budget envelope, in that 4 small landers could be delivered directly to Titan on a simple carrier from interplanetary approach (somewhat reminiscent of the Pioneer Venus probes). The small semi-hard landers would not need parachutes, legs nor sampling systems, and thus could be relatively simple and inexpensive. In the Entry-Descent-and-Landing (EDL) context, a Titan network mission is considerably easier than a corresponding Mars mission. It will be recalled that the 1.3m diameter, 200kg Huygens probe, with a 1.3m parachute, hit the ground at 5 m/s and was unaffected by the 15g impact. A 10-50kg small station, with a Huygens-like 5cm foam insulation layer, will encounter similar or lower impact speeds and loads without a parachute. The stations might be simple DS-2 or Huygens-like capsules, or perhaps with simple self-righting petals like the Russian Luna-9 or the Mars Pathfinder. Communication, of course, would be direct-to-Earth. The key science goals can be met with modest bandwidth (a Megabit per Titan day, or ~1 bps, is ample over year-long periods), compatible with low- or medium-gain transmission to the DSN, especially if the bandwidth is leveraged by intelligent data prioritization on the landers such as event-triggered sampling and data compression. UNQUOTE I have a queston regarding the range of arrival speed for which this could be done. Presumably when a very small payload is involved it is posible to send it on a much faster trajectory from Earth to its target than could be done for the likes of Cassini, should that be deemed worthwhile. I am wondering if Titan's atmosphere has an absolute maximum safe arrival speed? |
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Holder of the Two Leashes It all depends on how much of the probe weight you... Aug 25 2009, 02:34 PM
ngunn I dunno. That's about three times faster than ... Aug 25 2009, 08:47 PM
Holder of the Two Leashes QUOTE (ngunn @ Aug 25 2009, 03:47 PM) ...... Aug 26 2009, 02:03 PM
ngunn QUOTE (Holder of the Two Leashes @ Aug 26 200... Aug 26 2009, 02:12 PM
vjkane QUOTE (ngunn @ Aug 25 2009, 11:47 AM) I h... Aug 25 2009, 10:42 PM
Enceladus75 This looks like a great and very workable proposal... Aug 27 2009, 02:15 AM
stevesliva QUOTE (Enceladus75 @ Aug 26 2009, 09:15 P... Aug 27 2009, 03:28 AM
rlorenz QUOTE (stevesliva @ Aug 26 2009, 10:28 PM... Aug 27 2009, 04:20 AM
Holder of the Two Leashes QUOTE (rlorenz @ Aug 26 2009, 10:20 PM) T... Aug 27 2009, 02:14 PM
nprev Ralph, how much targeting accuracy could be practi... Aug 27 2009, 04:31 AM
stevesliva Bit of a facepalm on the Titan mass thing. At lea... Aug 27 2009, 05:36 AM
remcook Don't worry, atmospheric scale height is inver... Aug 27 2009, 07:07 AM![]() ![]() |
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