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Mission type | Reconnaissance |
---|---|
Operator | NASA/JPL |
Mission duration | ≥1.5 years [1] |
Spacecraft properties | |
Launch mass | ≈3,939 kg |
BOL mass | ≈2,000 kg [1] |
Dry mass | ≈1,110 kg |
Power | 290 W [1] |
Start of mission | |
Launch date | 2030 (suggested) |
Rocket | Atlas V 511 or SLS |
Uranus orbiter | |
Orbital insertion | 2041 |
Orbits | ≥14 (proposed) [1] |
OCEANUS (Origins and Composition of the Exoplanet Analog Uranus System) is a mission concept conceived in 2016 and presented in 2017 as a potential future contestant as a New Frontiers program mission to the planet Uranus. [2] [1] The concept was developed in a different form by the astronautical engineering students of Purdue University during the 2017 NASA/JPL Planetary Science Summer School. [3] OCEANUS is an orbiter, which would enable a detailed study of the structure of the planet's magnetosphere and interior structure that would not be possible with a flyby mission. [2]
Because of the required technology development and planetary orbital dynamics, the concept suggests a launch in August 2030 on an Atlas V 511 rocket and entering Uranus' orbit in 2041. [1]
Ice giant sized planets are the most common type of planet according to Kepler data. The little data available on Uranus, an ice giant planet, come from ground-based observations and the single flyby of the Voyager 2 spacecraft, so its exact composition and structure are essentially unknown, as are its internal heat flux, and the causes of its unique magnetic fields and extreme axial tilt or obliquity, [1] making it a compelling target for exploration according to the Planetary Science Decadal Survey. [2] [4] The primary science objectives of OCEANUS are to study Uranus' interior structure, magnetosphere, and the Uranian atmosphere. [1]
The required mission budget is estimated at $1.2 billion. [1] The mission concept has not been formally proposed to NASA's New Frontiers program for assessment and funding. The mission is named after Oceanus, the Greek god of the ocean; he was son of the Greek god Uranus. [5]
![]() | This section needs to be updated.(October 2024) |
Since Uranus is extremely distant from the Sun (20 AU), and relying on solar power is not possible past Jupiter, the orbiter is proposed to be powered by three multi-mission radioisotope thermoelectric generators (MMRTG), [2] [1] a type of radioisotope thermoelectric generator. As of 2015 [update] , there was enough plutonium available to NASA to fuel three more MMRTG like the one used by the Curiosity rover, one of which was already committed to the Perseverance rover. [6] [7] The other two have not been assigned to any specific mission or program, [7] and could be available by late 2021. [6] A second possible option for powering the spacecraft other than a plutonium powered RTG would be a small nuclear reactor powered by uranium, such as the Kilopower system in development as of 2019.
The trajectory to Uranus would require a Jupiter gravity assist, but such alignments are calculated to be rare in the 2020s and 2030s, so the launch windows will be scant and narrow. [2] To overcome this problem two Venus gravity assists (in November 2032 and August 2034) and one Earth gravity assist (October 2034) are planned along with the use of solar-electric propulsion within 1.5 AU. [1] The science phase would take place from a highly elliptical orbit and perform a minimum of 14 orbits. [1] If launching in 2030, reaching Uranus would occur 11 years later, in 2041, [1] and it would use two bipropellant engines for orbital insertion. [1]
Alternatively, the SLS rocket could be used for a shorter cruise time, [8] but it would result in a faster approach velocity, making orbit insertion more challenging, especially since the density of Uranus' atmosphere is unknown to plan for safe aerobraking. [7]
The 12.5 kg scientific payload would include instruments for a detailed study of the magnetic fields and to determine Uranus' global gravity field: [2] [1]