13:45 〜 14:00
[PPS01-01] Uranus Orbiter and Probe (UOP): The 2023–2032 Planetary Survey and Astrobiology Decadal Survey Mission Concept
★Invited Papers
キーワード: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.
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.