Sponsors + Partner Organizations
We are very thankful for the following organizations for making this summer’s program possible!
MINI-LUNA
Cislunar Asteroid Remote Sensing Mission
Mission Overview
The 12U Mini-Luna SmallSat will travel on a rideshare program on a Lunar Transfer Injection (LTI) to the Earth-Moon L2 (Lagrange) point. Mini-Luna will study the TCO using remote sensing composition analysis instruments, with an extended mission to redirect the TCO.
Mission Motivation
From the Decadal Surveys:
- Q1.2b How, Where, and When Did Radial Mixing and Segregation of Solids and Gas Occur in the Nebula?
- Q1.3c Which Reservoirs and Materials (Gas, Rock, Ice, Organics) Formed into Planetesimals?
- Q4.1b How Has Collisional and Dynamical Evolution Affected Small Body Populations?
- Q4.1c What Are the Life Cycles (Physical States and Rotational Properties) of Small Bodies in the Solar System and How Are They Affected by Collisions, Thermal Changes, and Non-gravitational Forces?
Mission Background: What are Mini-Moons?
Science Objectives
- Characterize internal structure of TCO
- Determine size, shape, and rotation rate of the TCO
- Characterize surface composition of materials, volatile compounds
Mission Storyboard
MINI-LUNA Spacecraft, TREX (TCO Rendezvous Explorer)
TREX rendezvous with a TCO and capture surface and tomographic imagery in order to analyze the target asteroid’s composition and structure.
Spacecraft overview:
- Stowed Size: 12U
- Total Mass: 22.4 kg
- Time to TCO 100 days
- Instruments: hyperspectral Imager, Low Frequency Radar (pictured below)
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