P077-0004
The Mars Orbiter for Resources, Ices, and Environments (MORIE) Mission Concept Study
Abstract:
These objectives are met by a payload complement of seven instruments: full polarization synthetic aperture radar (SAR), a dual-band radar sounder, a 1-m per pixel multiband imager, both short-wave and long-wave infrared spectrometers, dual stereo cameras, and a wide-angle imager. MORIE utilizes a large, SEP-powered spacecraft that drives the power requirement providing ample power to run the radar and telecommunications on orbit. A 2026 launch is baselined, requiring ~ 2 years to cruise to Mars and spiral down into an equator-crossing sun-synchronous orbit with an inclination of 92.7 degrees. The spacecraft spends a full Mars year in this orbit, then transitions to a 90-degree true-polar orbit to enable radar sounding of previously unobserved regions of the polar caps. The design does not present any major technical challenges or novel risks. The team costed both the full mission and, due to the recent programmatic interest in a Mars Ice Mapper, an ice-focused radar version. Cost models suggest the full mission point design is larger than the current New Frontiers cost cap without instrument or hardware contributions or further design maturity.