BLUESHIFT LLC — National Aeronautics and Space Administration SBIR Phase I: Z5
BLUESHIFT LLC — SBIR Phase I award from National Aeronautics and Space Administration.
Phase I SBIR feasibility signal
- Phase I awards fund proof-of-concept work. For capture teams, they mark early interest from National Aeronautics and Space Administration in a technical approach.
- Watch for Phase II follow-ons from the same firm/topic family — that conversion path is where budgets and transition pressure rise.
- Obligated amount $124,927. Cross-check similar awards in the same agency and technology tags for going-rate context.
- Topic code Z5 links this award to a solicitation family — search the same topic stem for incumbents and recompete timing.
- Amount
- $124,927
- Agency
- National Aeronautics and Space Administration
- Program / Phase
- SBIR · Phase I
- Topic
- Z5
- Solicitation
- SBIR_20_P1
- NAICS
- —
- Place of performance
- CO
- Period
- 2020-07-31 → 2021-03-01
Description
Blueshift, LLC doing business as Outward Technologies proposes to develop a Discrete Element Method (DEM) modeling framework using open-source software to simulate the combined thermal and mechanical interactions between rovers and regolith in Permanently Shadowed Regions (PSRs) at the lunar poles. This proposed set of numerical tools innovates on the current state of the art by explicitly solving for both thermal and mechanical interactions between rover components and regolith, and by the inclusion of volatiles such as water ice of multiple forms (e.g. vapor deposited ldquo;frostrdquo;, blocky deposits, and icy regolith mixtures) in a grain-based DEM model. Rover components including probes, drills, wheels, and soil sampling equipment will be simulated using coupled FEM software to reduce computation time. A coupled thermo-hydro-mechanical model will further be explored for its suitability in simulating volatile phase change and gas transport through cryogenic regolith as represented by a bonded-particle DEM. These numerical modeling capabilities will be integrated within a single, easy to use simulation framework for approximating thermal and mechanical interactions between rovers and regolith across ranges of possible conditions which may be encountered in and near PSRs on the Moon. These combined numerical tools will enable NASA and its partners to inexpensively evaluate hardware designs for lunar ISRU missions aimed at exploration and prospecting for volatiles. These improved modeling capabilities will further de-risk planned missions to the lunar south pole by identifying successful control strategies and hardware designs for ISRU sampling, material handling, increased rover operability, and surviving the lunar night, leading to more rugged and capable rovers for lunar polar missions while reducing their costs related to development and testing.