Astronomy:OCEANUS
| 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's orbit in 2041.[1]
Overview

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's 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]
Power and propulsion
| Parts of this astronomy (those related to section) need to be updated. Please update this astronomy to reflect recent events or newly available information. (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's atmosphere is unknown to plan for safe aerobraking.[7]
Payload

The 12.5 kg scientific payload would include instruments for a detailed study of the magnetic fields and to determine Uranus's global gravity field: [2][1]
- UMAG (Uranus Magnetometer) – is a magnetometer to study the magnetosphere and constrain models for dynamo generation.
- GAIA (Gravity and Atmospheric Instrument Antenna) – it would utilize the on-board communications antenna, transmitting in both X band and Ka band frequencies for radio science that would allow mapping Uranus's global gravity field.
- UnoCam (Uranus's Juno Cam) – is a visible light, color camera to detect navigation hazards in Uranus's ring system and to provide context and panoramic images.
- URSULA (Understanding Real Structure of the Uranian Laboratory of Atmosphere) – an atmospheric probe that would be jettisoned into the atmosphere of Uranus just before orbit insertion. It would descend under a parachute and measure the noble gas abundances, isotopic ratios, temperature, pressure, vertical wind profiles, cloud composition and density,[2] via a mass spectrometer, atmospheric structure instrument, nephelometer and ultra-stable oscillator. The total mass of the probe's instruments is about 127 kg.[1]
See also
- Uranus mission proposals
References
- ↑ 1.00 1.01 1.02 1.03 1.04 1.05 1.06 1.07 1.08 1.09 1.10 1.11 1.12 1.13 1.14 1.15 Bramson, A. M; Elder, C. M; Blum, L. W; Chilton, H. T; Chopra, A; Chu, C; Das, A; Delgado, A et al. (2017). "OCEANUS: A Uranus Orbiter Concept Study from the 2016 NASA/JPL Planetary Science Summer School". 48th Lunar and Planetary Science Conference 48 (1964): 1583. Bibcode: 2017LPI....48.1583B.
- ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 Elder, C. M; Bramson, A. M; Blum, L. W; Chilton, H. T; Chopra, A; Chu, C; Das, A; Davis, A et al. (2017). "New Frontiers-Class Missions to the Ice Giants". Planetary Science Vision 2050 Workshop 1989: 8147. Bibcode: 2017LPICo1989.8147E.
- ↑ Mansell, J.; Kolencherry, N.; Hughes, K.; Arora, A.; Chye, H.S.; Coleman, K.; Elliott, J.; Fulton, S. et al. (2017). "Oceanus: A multi-spacecraft flagship mission concept to explore Saturn and Uranus". Advances in Space Research (Elsevier BV) 59 (9): 2407–2433. doi:10.1016/j.asr.2017.02.012. ISSN 0273-1177.
- ↑ "Lean U.S. missions to Mars, Jupiter moon recommended". 7 March 2011. Reuters. 8 March 2011. https://www.reuters.com/article/us-space-usa-future-idUSTRE7266XJ20110308.
- ↑ OCEANUS: A Concept Study (PDF) – poster. 2017.
- ↑ 6.0 6.1 Leone, Dan (11 March 2015). "U.S. Plutonium Stockpile Good for Two More Nuclear Batteries after Mars 2020". Space News. http://spacenews.com/u-s-plutonium-stockpile-good-for-two-more-nuclear-batteries-after-mars-2020/.
- ↑ 7.0 7.1 7.2 Moore, Trent (12 March 2015). "NASA can only make three more batteries like the one that powers the Mars rover". Blastr. http://www.blastr.com/2015-3-12/nasa-can-only-make-three-more-batteries-one-powers-mars-rover.
- ↑ Mansell, J; Kolencherry, N; Hughes, K; Arora, A; Chye, H.S; Coleman, K; Elliott, J; Fulton, S et al. (2017). "Oceanus: A multi-spacecraft flagship mission concept to explore Saturn and Uranus". Advances in Space Research 59 (9): 2407–33. doi:10.1016/j.asr.2017.02.012. Bibcode: 2017AdSpR..59.2407M.

