Why This Mission?
SCIM will fundamentally advance our knowledge of the geology, climate, and habitability of Mars; a terrestrial planet that may have been similar to Earth in its early history. It will also help us to prepare for future human exploration by providing detailed, particle-by-particle analysis of the ubiquitous Martian dust -- and its possible hazards to human explorers, their habitat, and equipment.
Mission Development
Phase 1: Detailed Design & Mission Optimization
SCIM is a mature mission concept and ready to go. We are currently fundraising to begin implementation. Our first phase entails detailed design and optimization work, with a special focus on the dust collector and sample return capsule.
In the early phase of SCIM development, work will focus on:
Optimizing the science plan using the latest data from Mars
Incorporating the most advanced flight avionics
Creating a detailed build plan and schedule to get us to the launch pad
Inking initial agreements with our SCIM partners including aerospace companies, our launch vehicle provider, universities and NASA
Updating mission costs using our revised management approach.
Sampling Mars
With a baseline launch opportunity in late 2024, SCIM performs a daring high-speed atmospheric pass down to below 40 km altitude timed to coincide with seasonal Martian dust storms, collecting thousands of Martian dust particles from the atmosphere. After the sample collection pass at Mars, the spacecraft returns directly to Earth, where its precious, sterilized samples descend by parachute to the ground.
2024 Mission Profile (Tentative)
Launch 9/18/2024
Mars Flyby 10/8/2025, Ls=152
Periapsis Altitude=40 km
Periapsis Velocity= 5.65 km/s
Periapsis Latitude= -47 degrees
LTST at Periapsis ~ 1:20 PM
Nominal DSM DV = 0 m/s
Earth Return 6/16/2027
Earth Entry V = 11.4 km/s
The Science & Technology
Advancing Our Understanding of Mars with Unique Data
As the first sample return from another terrestrial planet, SCIM will provide a unique data set and a comparative basis for understanding how the rocky inner planets formed and why they have evolved so differently from each other.
Science Objectives for SCIM Mission
Quantitatively characterize the chemical, isotopic, and mineralogical composition of Martian crustal materials as represented by the global dust
Investigate aqueous alteration processes and environments that have affected or produced Martian surface materials
Understand Mars’ volatile reservoirs and hydrologic cycles
Synthesize data from remote-sensing and Earth-based laboratory investigations of Martian materials to provide “ground truth” for past and future missions
Dust Collector and Sample Return Capsule
Early hardware builds will help SCIM make key progress towards the launch pad. We propose early prototypes and ultimately early flight builds of both the aerogel-based dust collector and the sample return capsule that will bring the Mars dust safely back to Earth.
Both of these key elements of SCIM provide naming opportunities for donors.
Fine Particle Studies Only Possible in Earth-based Labs
Fine particles, in particular, can record many interesting and varied processes on Mars, from aqueous transport to volcanic eruptions. By studying the fine particles in atomic-level detail only possible in labs on Earth, we will provide never-before seen insights into the most important processes that have shaped Mars. These insights will also help engineers design more robust mechanisms, habitats and space suits in future robotic and crewed missions to the surface of Mars.
Slicing Dust Particles Using Nanotechnology
SCIM leverages the very latest in nano-science and technology available here on Earth. Scientists in terrestrial labs have the ability to slice a single microscopic dust particle into numerous pieces that can be shipped around the globe for analyses in the most advanced labs on Earth.
Advantages of Dust Sample Return Mission
High Science Return
Material origin and processing are recorded at microscopic, molecular, and atomic levels—scales readily accessible only by Earth-based lab instruments
Important scientific discoveries can be rapidly confirmed by new measurements with additional instruments
Curated samples are available when new hypotheses arise and call for new measurements
Advanced Instrumentation
The very best instruments are used for samples analysis: no limitation on what can be “flight qualified” by the time of launch
No time limits: As more advanced instruments are developed, they can be used on the curated sample
Participation
Hundreds of scientists and students can participate directly in the mission by making measurements in their own labs—literally dozens of highly sophisticated instruments worldwide will be used
Many scientists not currently part of the traditional “Mars science community” will be involved—these scientists will provide valuable new perspectives and ideas
Millions of Mars enthusiasts will have access to SCIM mission imagery and science results, and we will enlist citizen scientists to help identify dust tracks in the aerogel, as well as participate in other aspects of the scientific analysis
Replication
Important results can be verified independently using the same method in another lab or by using a complementary technique
Experimental anomalies can be directly resolved
Aeropass & Aeroshell Instrumentation
Using a sleek, elongated aeroshell, SCIM will race through the Martian atmosphere collecting samples, but won’t be captured into orbit. Instead, after emerging from the atmospheric pass SCIM will return directly to Earth with its treasure. The cone-shaped aeroshell is similar to geometries of planned Mars human landing systems, and instrumenting the aeroshell with sensors will provide critical pathfinder data for future human explorers.
SCIM’s sample capture is based on the successful collection system for the Stardust mission (shown above), using cells filled with ultra-light aerogel to capture and preserve the dust particles. Aerogel is both strong and heat resistant and provides perfect protection for SCIM’s Martian cargo.
Captured particles are slowed in the aerogel and come to rest at the tip of a carrot-shaped track, with the track pointing the way. In this image from a test, the particle is at the upper right.
Heating levels on the aeroshell are estimated with cutting edge computational models, and anchored to reality through wind tunnel testing. These images show the results of such tests (left) and calculations (right). As expected, heating levels near the aeroshell nose are highest, while the rear of the spacecraft stays much cooler.
Extensive modeling and experiments by the SCIM team have shown that small particles easily traverse the atmospheric shock wave and reach the collection system, which is located near the rear of the spacecraft where temperatures are relatively cool. The design of the collection system will result in minimal heating of the dust particles during the capture process in order to maximize science return.
Tested and Ready
Testing on Earth and high end computational models have guided SCIM’s design to ensure that particles will reach our aerogel collectors and that heating levels are low to ensure the sampling system and particles preserve the best science.
The flight system design is mature, and NASA experts have previously deemed development plans low risk.
Educational Opportunities to Join SCIM
We are building plans for education programs to engage people around the world in the SCIM journey, including a student-built experiment and hosting secondary payloads such as cubesats.
Student-built Experiment and Secondary Payloads
Education and public engagement are important to the SCIM journey. Enabling meaningful participation through hands-on activities — such as creating SCIM’s dust counter and possibly cubesats to be released at Mars — will have a positive impact on preparing future generations for careers in technological fields. Near-term work involved detailed accommodation studies to maximize the number of student experiments SCIM can carry. It will also support initial competitions and designs of SCIM’s student experiments.