Japan Geoscience Union Meeting 2024

Presentation information

[E] Oral

P (Space and Planetary Sciences ) » P-PS Planetary Sciences

[P-PS01] Outer Solar System Exploration Today, and Tomorrow

Tue. May 28, 2024 1:45 PM - 3:15 PM 103 (International Conference Hall, Makuhari Messe)

convener:Jun Kimura(Osaka University), Kunio M. Sayanagi(NASA Langley Research Center ), Fuminori Tsuchiya(Planetary Plasma and Atmospheric Research Center, Graduate School of Science, Tohoku University), Chairperson:Yasumasa Kasaba(Planetary Plasma and Atmospheric Research Center, Tohoku University), Jun Kimura(Osaka University)

1:45 PM - 2:00 PM

[PPS01-01] Uranus Orbiter and Probe (UOP): The 2023–2032 Planetary Survey and Astrobiology Decadal Survey Mission Concept

★Invited Papers

*Ian J Cohen1, Amy Simon2, Francis Nimmo3, Debra Buczkowski1, Richard C Anderson1, Robert E Gold1, Art Azarbarian1, Debarati Chattopadhyay1, Max Harrow1, Juan Arrieta4, Martin T Ozimek1, Andrew B Calloway1, Christopher J Scott1, Alice F Bowman1, Patrick A McCauley1, Helen H Hwang1, Dinesh Kumble Prabhu5, Gary A Allen, Jr5, Joshua Monk5, Soumyo Dutta6, John M Thornton5, Alejandro R Pensado6, David Coren7, Kimberly A Slack1, Katherine L Rorschach1, Hari Nair1, Jeremy W John1, Erich K Schulze1, Dave R Weir1, Bruce Williams1, Reza Ashtari1, Daniel T Gallagher1, John H Wirzburger1, Rebecca C Foust1, Kirk N Volland1, Steve S Cho1, Christian Campo1, Justin W Kelman1, Adrian Hill1, Vincent Bailey1, Jackie W Perry1, Elliott Rodberg1, Michelle Mary Donegan1, Faith Kahler1, Kathy Kha1 (1.Johns Hopkins University Applied Physics Laboratory, 2.NASA Goddard Space Flight Center, 3.University of California, Santa Cruz, 4.Nabla Zero Labs, 5.NASA Ames Research Center, 6.NASA Langley Research Center, 7.NASA Jet Propulsion Laboratory)

Keywords:Uranus, Decadal Survey, mission

Uranus Orbiter and Probe (UOP) is a Flagship-class mission concept developed in response to the 2023–2033 Planetary Science and Astrobiology Decadal Survey and endorsed as the highest-priority new flagship mission. UOP was developed with the aim of answering the top-level science questions concerning the Uranus system. The mission deploys an atmospheric probe into Uranus shortly after orbit insertion, followed by multiple flybys of Titania to reduce the orbital inclination to the equatorial plane, carrying out observations of the planet as it does so. An equatorial tour of all five major moons follows, completing a 4.5-year science mission phase at Uranus. The modest payload baselined was selected to address the top-priority science questions concerning Uranus’s atmosphere, interior, magnetosphere, rings and small satellites, and large satellites.

The objective of this study was to update the prior Uranus Orbiter and Probe concepts, including a project start between 2023–2030, with refined science goals and payload complement, updated launch vehicles, and a chemical-only mission design. The study was also directed to increase concept maturity/fidelity where possible, at a concept maturity level (CML) of 4.

Alternative Earth-to-Uranus interplanetary trajectories were analyzed to satisfy multiple, competing objectives. Numerous options were identified for launches throughout the 2030s, taking advantage of newer, higher-performing launch vehicles. Optimal launches use a Jupiter gravity assist (JGA) to achieve the most cost-efficient solution; however, numerous other viable alternatives without JGA exist, either with modestly increased flight times or the use of Venus. Significant emphasis was placed on optimizing the atmospheric probe deployment while developing an integrated, end-to-end trajectory from launch through disposal, in response to technical feedback from previous ice giant concept studies.

As a flagship mission, UOP has the imprimatur of a broad community. The mission would answer fundamental questions about the origin and evolution of our own solar system, and the characteristics of planets elsewhere. The mission concept requires no new technologies or launch vehicle, and has a highly flexible tour design and ample mass and power margins.