BLUESHIFT LLC — National Aeronautics and Space Administration SBIR Phase I: Z12
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 $124,907. Cross-check similar awards in the same agency and technology tags for going-rate context.
- Topic code Z12 links this award to a solicitation family — search the same topic stem for incumbents and recompete timing.
- Amount
- $124,907
- Agency
- National Aeronautics and Space Administration
- Program / Phase
- SBIR · Phase I
- Topic
- Z12
- Solicitation
- SBIR_20_P1
- NAICS
- —
- Place of performance
- CO
- Period
- 2020-07-24 → 2021-03-01
Description
NASA is requesting technologies for efficient transmission of energy for oxygen/metal extraction. Blueshift proposes to develop a continuous feed reactor for rapidly heating lunar regolith to prescribed temperatures exceeding 2,200deg; C using Concentrated Solar Power (CSP) more efficiently than current state of the art and extracting oxygen through two extraction processes (carbothermal reduction, vapor phase pyrolysis). This Solar Concentrating Oxygen Reactor for Continuous Heating and Extrusion of Regolith (SCORCHER) implements Blueshiftrsquo;s patent pending CSP thermal control technology for providing process specific temperatures, an innovative reactor design to bring regolith up to temperature and extract oxygen more efficiently, and a continuous slag extrusion design enabling continuous processing and byproduct utilization as a crude fabrication material for casting, construction, and additive manufacturing. Benefits of the proposed innovation include a 1.7kW reduction in power requirements compared to an equivalent microwave-heated pyrolysis system, continuous oxygen extraction capability, reduced processing times, increased oxygen yields, high temperature pyrolysis capability (gt;2000deg; C) for direct oxygen extraction without a gas reactant, extraction process agnostic design for wide adaptability, temperature ramping to mitigate temperature shock failure in components, and secondary resource utilization of extruded slag for part fabrication, long duration thermal energy storage, or for secondary smelting and refining. The Phase I effort will focus on reactor design and prototype development, optical system and reactor modeling, and characterization testing using the prototype reactor to perform carbothermal reduction and vapor phase pyrolysis on lunar soil simulant JSC-1A.