Title:
Titan/Saturn System Mission 2008: Exploring Titan on a Budget (and Without Aerocapture!)

dc.contributor.author Elliott, John O. en_US
dc.contributor.author Lunine, Jonathan en_US
dc.contributor.author Reh, Kim en_US
dc.contributor.author Strange, Nathan en_US
dc.contributor.author Spilker, Tom en_US
dc.contributor.corporatename California Institute of Technology en_US
dc.contributor.corporatename University of Arizona. Lunar and Planetary Laboratory en_US
dc.contributor.corporatename Jet Propulsion Laboratory (U.S.)
dc.date.accessioned 2009-01-20T20:13:35Z
dc.date.available 2009-01-20T20:13:35Z
dc.date.issued 2008-06-24
dc.description This presentation was part of the session : Probe Missions to the Giant Planets, Titan and Venus en_US
dc.description Sixth International Planetary Probe Workshop en_US
dc.description.abstract Titan has been the topic of a number of mission studies in recent years, culminating in the 2007 Titan Explorer flagship mission study led by APL with JPL participation. This study, as with those previous, made use of the favorable conditions of Titan's atmosphere to allow aerocapture directly into Titan orbit, a technique which would provide over 6 km/s delta-V capability, greatly increasing delivered mass to Titan when compared to purely propulsive options. This year NASA has chosen to continue study of a Titan/Saturn System Mission, but with new ground rules that encourage a quick flight time to Titan while precluding the use of aerocapture. Further direction includes performing Saturn system science (including Enceladus) in addition to purely Titan-focused investigations, as well as a requirement to provide accommodation for a European-provided in-situ vehicle that would be delivered to Titan by the orbiter spacecraft. The financial cap for the US portion of the mission has been set at $2.1B (FY07). The sum of these constraints has resulted in a complete redesign of the Titan mission and flight system, the most notable changes being driven by the necessity of providing a large onboard chemical delta-v capability to take the place of aerocapture. Responding to these constraints, the JPL-APL-ESA/ESTEC team has developed a concept that meets study ground rules and provides an extremely valuable post-Cassini exploration of Titan and the Saturn system. This paper presents an introduction to the challenges, the trades and the resulting mission and flight system concept being developed for this potential outer planets flagship mission. en_US
dc.description.sponsorship NASA en_US
dc.identifier.uri http://hdl.handle.net/1853/26409
dc.publisher Georgia Institute of Technology en_US
dc.relation.ispartofseries IPPW08. Probe Missions to the Giant Planets, Titan and Venus en_US
dc.subject Titan mission en_US
dc.subject Mission architecture en_US
dc.subject Spacecraft design en_US
dc.title Titan/Saturn System Mission 2008: Exploring Titan on a Budget (and Without Aerocapture!) en_US
dc.type Text
dc.type.genre Proceedings
dspace.entity.type Publication
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename College of Engineering
local.relation.ispartofseries International Planetary Probe Workshop (IPPW)
relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
relation.isSeriesOfPublication 6369d36f-9ab2-422f-a97e-4844b98f173b
Files
Original bundle
Now showing 1 - 2 of 2
Thumbnail Image
Name:
95-150-1-PB.pdf
Size:
3.14 MB
Format:
Adobe Portable Document Format
Description:
PDF Presentation
No Thumbnail Available
Name:
95-198-1-PB.ppt
Size:
4.99 MB
Format:
Microsoft Powerpoint
Description:
Power Point Presentation
Collections