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The Award database is continually updated throughout the year. As a result, data for FY21 is not expected to be complete until September, 2022.

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. Multiscale Eulerian-Lagrangian Spray Methodology Coupled with Flamelet Models for Liquid Rocket Engine Combustion

    SBC: STREAMLINE NUMERICS, INC.            Topic: T9

    The innovation proposed here is a novel multi-scale coupling methodology implemented in the Loci-STREAM CFD code, for developing a high-fidelity, high-performance multiphase combustion modeling capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/Methane) in liquid rocket engines (LREs). During Phase 1 work, a ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  2. MarsOasis- An Efficient Autonomously Controlled Martian Crop Production System

    SBC: Space Lab Technologies, LLC            Topic: T7

    The MarsOasis™ cultivation system is a versatile, autonomous, environmentally controlled growth chamber for food provision on the Martian surface. MarsOasis™ integrates a wealth of prior research and Mars growth chamber concepts into a complete system design and operational prototype. MarsOasis™ includes several innovative features relative to the state of the art space growth chambers. I ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  3. Multi-Band Software Defined Radio Sensor System

    SBC: Pegasense, LLC            Topic: T13

    This Multiband Software Defined Radio (SDR) sensor system proposal will demonstrate the ability to operate within multiple frequency bands and across multiple technology platforms in a single transceiver. The center frequencies and bandwidths chosen are representative of current demonstrated commercial or research devices and bands used: 400 MHz, 900 MHz, and 2.4 GHz ISM bands, with bandwidths of ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  4. Wireless Passive Nanoparticle based Intelligent Sensor System for Extreme Environments

    SBC: Sensatek Propulsion Technology, Inc.            Topic: T13

    Sensatek Propulsion Technology, Inc. proposes to demonstrate the feasibility of a wireless, passive, nanoparticle-based sensor system. The sensor in its current form can be used to measure real time temperatures and pressures wirelessly without the need of an external energy source. It should be noted that the same sensing principle can be used for strain monitoring as well. It comprises of a micr ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  5. A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin

    SBC: REACTION SYSTEMS, INC            Topic: T6

    Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal assembly (CDRA). While it has performed well on the ISS, managers have concluded that using the device to reach the new ppCO2 limit of 2.0 mm Hg is not practical and a new method is needed.In this projec ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  6. Extensible Modeling to Create Knowledgebase for AM Processing of Alloy GrCop-84

    SBC: Applied Optimization, Inc            Topic: T12

    The research objective of the proposed work is to demonstrate feasibility of utilizing extensible modeling to create an AM knowledgebase for copper alloy, GrCop-84, and utilize it to design an AM process for GrCop-84. The work plan has three tasks: (1) Utilize process modeling to demonstrate feasibility of predicting AM process parameters for alloy GrCop-84 for the powder bed and blown powder proc ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  7. Aeroservoelastic Multifidelity Design of Biomimetic Aircraft (AMuBA)

    SBC: INTELLIGENT AUTOMATION, INC.            Topic: T15

    NASA has been investigating morphing aircraft for multi-mission capabilities and performance improvements in existing fixed-wing aircraft. In addition, the design of aeroelastic aircraft that can control the structural flexibility to their advantage, is an open area of research and development. In spite of the plethora of work on morphing aircraft and long slender wings, the goal of fielding such ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  8. Additive Manufacture of Refractory Metal Propulsion Components

    SBC: Geoplasma, LLC            Topic: T9

    Niobium alloy (C-103) reaction control system (RCS) chambers have been used on numerous NASA programs. However at elevated temperatures, the strength of C-103 decreases significantly. Higher strength niobium alloys have been developed, but these alloys lack the formability of C-103. Recently, Additive Manufacture (AM) of niobium and C-103 has been demonstrated using powder bed electron beam me ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  9. Validated Engineering Tools for Thin-Ply Composites

    SBC: Opterus Research and Development, Inc.            Topic: T12

    Opterus Research and Development, Inc. proposes to develop and validate multi-scale thin-ply High Strain Composites (HSCs) constitutive modeling tools for incorporation into commercial finite element analysis codes. The constitutive models will capture the time-temperature-load-deformation viscoelastic characteristics common to HSCs as well as the yielding or permanent deformation associated with ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  10. Prediction of Plume Induced Rock Fracture for Landers

    SBC: CFD Research Corporation            Topic: T9

    The landing surface damage and liberation of debris particles caused by rocket plume impingement flow during spacecraft propulsive landing on unprepared surfaces of Moon, Mars, and other celestial bodies poses a high risk for robotic and human exploration activities. Simply determining whether the plume induced loads exceed the bedrock bearing capacity threshold is not sufficient. An integrated m ...

    STTR Phase I 2018 National Aeronautics and Space Administration
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