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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

  1. Highly Efficient Closed-Loop CO2 Removal System for Deep-Space ECLSS

    SBC: TDA Research, Inc.            Topic: T6

    TDA Research Inc.(TDA) in collaboration with University of Puerto Rico – Mayaguez (UPRM is proposing to develop a highly efficient CO2 removal system based on UPRM proprietary strontium exchanged silico-alumino-phosphate (Sr-SAPO-34) sorbent for closed loop space craft cabin air re-vitalization during deep space missions. In the Phase I work, we successfully completed bench-scale proof-of-concep ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  2. uG-LilyPond- Floating Plant Pond for Microgravity

    SBC: Space Lab Technologies, LLC            Topic: T7

    Regenerative space life support will undoubtedly require food production, to recover nutrients and close the carbon loop in a spacecraft habitat. Aquatic plants have enormous potential for edible biomass production but have been little studied as potential food crops for space applications. The proposed μG-LilyPond™ is an autonomous environmentally controlled floating plant cultivation system ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  3. Highly Sensitive Flash LADAR Camera

    SBC: VOXTEL, INC.            Topic: T9

    To address the urgent need for 3D flash-lidar technology for landing on solar system bodies and for spacecraft rendezvous and docking with satellites, an effort is proposed to fabricate, characterize, and test a versatile, high-sensitivity InGaAs APD 3D flash lidar and to advance the technology-readiness level (TRL) of lidar technologies suitable for NASA mission requirements. Leveraging an existi ...

    STTR Phase II 2019 National Aeronautics and Space Administration
  4. Efficient cFS-based On-board Lamberts Solution for DSMs

    SBC: Advanced Space LLC            Topic: T11

    Distributed Spacecraft Missions (DSM) architectures provide unique scientific and programmatic benefits including multipoint in-situ measurements, multi-angle viewpoints, and improved understanding of the connections between separately measured phenomena and their time variations. However, these missions impose significant operational demands on ground tracking resources and mission operators alik ...

    STTR Phase II 2019 National Aeronautics and Space Administration
  5. Transient Acoustic Environment Prediction Tool for Launch Vehicles in Motion During Early Lift-Off

    SBC: CFD Research Corporation            Topic: T1

    Launch vehicles experience extreme acoustic loads dominated by rocket plume interactions with ground structures during liftoff, which can produce damaging vibro-acoustic loads on the vehicle and payloads if not properly understood and mitigated against. Existing capabilities for modeling turbulent plume physics are too dissipative to accurately resolve the acoustic propagation and detailed vehicle ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  6. Multiphase Modeling of Solid Rocket Motor Internal Environment

    SBC: CFD Research Corporation            Topic: T1

    Solid rocket motor (SRM) design requires detailed understanding of the slag accumulation process in order to: predict thrust continuity, optimize propellant conversion efficiency, predict coning effects from sloshing, and to assess potential orbital debris (slag) hazard. Current state-of-the-art models for SRM environment do not have the capability to simulate the accumulation and dynamics of slag ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  7. Launch Weather Decision Support System

    SBC: Radiometrics Corporation            Topic: T1

    NASA wants a cost-effective atmospheric remote sensing system providing accurate temperature and humidity profiles to least 10 km height in clear and cloudy conditions. Radiometrics Microwave Profiler (MP) products currently provide accurate temperature and humidity profiles in good agreement with radiosondes to 3 km height. Good agreement can be extended beyond 10 km height using variational retr ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  8. An Additive Manufacturing Technique for the Production of Electronic Circuits

    SBC: MORNINGBIRD MEDIA CORPORATION            Topic: T12

    Under the support of a FY 2016 NASA Phase I Small Business Technology Transfer (STTR) contract (NASA contract number NNX16CM40P), Morningbird Media Corporation in collaboration with Alabama A&M University Research, Innovation in Science and Engineering (AAMU-RISE) Foundation, has devised a unique method for an additive manufacturing technique for the direct 3D printing of functional electronics. T ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  9. A Self-Regulating Freezable Heat Exchanger for Spacecraft

    SBC: TDA Research, Inc.            Topic: T601

    A spacecraft thermal control system must keep the vehicle, avionics and atmosphere (if crewed) within a defined temperature range. Since water is non-toxic and good for heat transport, it is typically used as the coolant that circulates within the crew cabin boundary. This loop then interfaces with another low freeze point fluid, such as ammonia, for transport of heat to a radiator where the tempe ...

    STTR Phase II 2013 National Aeronautics and Space Administration
  10. High-Fidelity Gas and Granular Flow Physics Models for Rocket Exhaust Interaction with Lunar Soil

    SBC: CFD Research Corporation            Topic: T701

    Current modeling of Lunar and Martian soil erosion and debris transport caused by rocket plume impingement lacks essential physics from the peculiar granular characteristics of highly irregular regolith particles. Current granular mechanics models are based on mono-disperse spherical particles empiricism unsuitable for capturing the poly-disperse irregularly shaped grain mechanics. CFDRC and the U ...

    STTR Phase II 2010 National Aeronautics and Space Administration
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