The Jupiter Icy Moons Orbiter (JIMO) was a proposed NASA spacecraft designed to explore the icy moons of Jupiter. The main target was Europa, where an ocean of liquid water may harbor alien life. Ganymede and Callisto, which are now thought to also have liquid, salty oceans beneath their icy surfaces, were also targets of interest for the probe.
The JIMO spacecraft
JIMO was to have a large number of revolutionary features. Throughout its main voyage to the Jupiter moons, it was to be propelled by an ion propulsion system via either the High Power Electric Propulsion or NEXIS engine, and powered by a small fission reactor. A Brayton power conversion system would convert reactor heat into electricity. Providing a thousand times the electrical output of conventional solar- or radioisotope thermoelectric generator (RTG)-based power systems, the reactor was expected to open up opportunities like flying a full scale ice-penetrating radar system and providing a strong, high-bandwidth data transmitter.
Using electric propulsion (8 ion engines, plus Hall thrusters of varying sizes) would make it possible to go into and leave orbits around the moons of Jupiter, creating more thorough observation and mapping windows than exist for current spacecraft, which must make short fly-by maneuvers because of limited fuel for maneuvering.
The design called for the reactor to be positioned in the tip of the spacecraft behind a strong radiation shield protecting sensitive spacecraft equipment. The reactor would only be powered up once the probe was well out of Earth orbit, so that the amount of radionuclides that must be launched into orbit is minimized. This configuration is thought to be less risky than the RTGs used on previous missions to the outer Solar System.
The Europa Lander Mission proposed to include on JIMO a small nuclear-powered Europa lander. It would travel with the orbiter, which would also function as a communication relay to Earth. It would investigate Europa's habitability and assess its astrobiological potential by confirming the existence and determining the characteristics of water within and below Europa's icy shell.
Northrop Grumman was selected on September 20, 2004 for a US$400 million preliminary design contract, beating Lockheed Martin and Boeing IDS. The contract was to have run through to 2008. Separate contracts, covering construction and individual instruments, were to be awarded at a later date.
Preliminary design specifications
Gross mass in low Earth orbit: 36,375 kg
Mass of xenon propellant: 12,000 kg
Reactor module mass: 6,182 kg (200 kWe output) Spacecraft module dry mass: 16,193 kg Science payload mass: 1,500 kg Electric turboalternators: multiple 104 kW (440 V AC) Deployable radiator: 422 m2 surface area Electric Herakles ion thrusters: multiple 30 kW high efficiency, specific impulse 7,000 s (69 kN·s/kg) Hall thrusters: high power, higher thrust Telecommunications link: 10 Mbit/s (4×250 watt TWTA) Deployed size: 58.4 m long × 15.7 m wide Stowed size: 19.7 m long × 4.57 m wide Mission design life: 20 years Launch date: 2017 Launch Vehicle: Delta IV Heavy Cost: 16 billion $ excluding launch
Nuclear propulsion
The JIMO mission was proposed to include a nuclear electric propulsion system for the long-duration mission, with power provided by a small 200 kWe fission power system. The nuclear propulsion program was conducted from 2003 to 2005 by the Naval Reactors branch of the DOE.
The proposed system design was a gas-cooled reactor and Brayton power conversion to generate a peak output of 200 kilowatts of power over the long life of the JIMO mission.
Mission profile
Three launches were planned for May 2015 to LEO in order to assemble the two transfer stages and the probe. Transfer stages were designed to launch the probe on its trajectory to Jupiter during the launch window extending from late October 2015 to mid-January 2016.
During the first month of flight, the probe's main structures would be deployed, the nuclear reactor activated, and the thrusters tested. The interplanetary flight would have lasted until April 2021 (the ion engines were supposed to work two-thirds of the time).
Once the probe was in the influence area of Jupiter, the navigation would become more complex and difficult. The probe would have to use gravity assist maneuvers to enter orbit.
The probe would have studied Callisto and then Ganymede for three months each, and finally Europa for one month (studies of Io were also planned when the orbital conditions would have been favorable).
At the end of the mission in September 2025, the vehicle would have been parked in a stable orbit around Europa.