Names | JIMO |
---|---|
Mission type | Jupiter orbiter |
Operator | NASA |
Mission duration | Cancelled |
Spacecraft properties | |
Manufacturer | Northrop Grumman |
Launch mass | Total (fully assembled): 36,375 kg (80,193 lb) |
Dry mass | Spacecraft module: 16,193 kg (35,699 lb) Reactor module: 6,182 kg (13,629 lb) |
Payload mass | 1,500 kg (3,300 lb) |
Dimensions | Fully deployed: 58.4 × 15.7 m (192 × 52 ft) |
Power | 200 kilowatts |
Start of mission | |
Launch date | NET May 2015 – January 2016 Planned |
Rocket | Delta IV Heavy Baseline (2005) |
Launch site | Cape Canaveral SLC-37B |
Jupiter orbiter | |
Orbital insertion | April 2021 Planned |
Orbital departure | September 2025 Planned |
Europa orbiter | |
Orbital insertion | September 2025 Planned |
Transponders | |
Bandwidth | 10-Mbit/s |
TWTA power | 4 x 250 watts |
Large Strategic Science Missions Planetary Science Division |
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.