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Award Data
The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.
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.
The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.
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Additive Manufacture of Refractory Metal Propulsion Components
SBC: GEOPLASMA LLC Topic: T9Niobium 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 -
Additive Manufacturing Sensor Fusion Technologies for Process Monitoring and Control.
SBC: ARCTOS Technology Solutions, LLC Topic: DLA18A001Universal Technology Corporation (UTC) has teamed with the University of Dayton Research Institute (UDRI), Stratonics, and Macy Consulting to demonstrate not only the transitionability into commercial systems, but also to develop the data analytics and monitoring and control requirements to extract the full value fromseveral sensors, including the Stratonics ThermaViz, acoustic and profilometry se ...
STTR Phase I 2018 Department of DefenseDefense Logistics Agency -
Advanced Li/CFx Primary Batteries with Non-Flammable Electrolytes
SBC: CFX BATTERY, INC. Topic: T601NASA seeks to develop high specific energy primary batteries that are safe and capable of performing under a wide temperature range, for manned space missions. To meet this goal, CFX Battery Inc. proposes to develop, characterize, and establish technological feasibility of a new Li/SF-CFx based high capacity lithium primary battery that offers higher rate capability and enhanced safety than conven ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization
SBC: AMERICAN GNC CORPORATION Topic: T1In providing an innovative solution to improving information technologies and health management systems, AGNC is proposing a significant technological achievement with the Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization. During in-flight conditions, this system is able to not only provide the status of information such as regarding the flight envel ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems
SBC: STREAMLINE NUMERICS, INC. Topic: T901The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b) flamelet modeling for turbulent combustion incorporated in a pr ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Air Vehicle Gust Response analysis for Conceptual Design
SBC: RESEARCH IN FLIGHT LLC Topic: T15Research in Flight (RIF) and Auburn University are offering the development of an advanced, robust tool and methodology that allows the simulation and modeling of gust and wake vortex encounters for Distributed Electric Propulsion (DEP) enabled Urban Air Mobility (UAM) vehicle concepts. DEP enabled UAM concepts offer the potential for large performance improvements by exploiting favorable synergie ...
STTR Phase I 2019 National Aeronautics and Space Administration -
A Modular In-Situ Curing Apparatus for Thermoset Resin Mixtures Applied as Thermal Protection Systems
SBC: INTELLIGENT OPTICAL SYSTEMS, INC. Topic: T12Future human extraterrestrial missions will require export and landing of countless payloads on the lunar and Martian surfaces. Such a quantity and rate of payload delivery will require cost-effective and rapid manufacturing of many large Thermal Protection Systems (TPS). IOS proposes to develop a modular system for in-situ bonding and curing of thermoset resin to the spacecraft structure to facil ...
STTR Phase I 2019 National Aeronautics and Space Administration -
An LED-Based Solar Simulator for Research, Development, and Testing of Photovoltaic Space Power Systems
SBC: Angstrom Designs, Inc. Topic: T201Solar cells are the critical power source for the majority of space missions. The advancement from single junction silicon cells to current, state-of-the-art, triple junction, germanium cells enabled greater mission power per weight, stowed volume and deployed area. Near-term, advanced solar cell technologies will range from 4 to 6 junctions, and include a variety of band gaps.Solar cell testing ...
STTR Phase I 2013 National Aeronautics and Space Administration -
A Scalable Gas-Particle Flow Simulation Tool for Lander Plume-Surface Interaction and Debris Prediction
SBC: CFD RESEARCH CORPORATION Topic: T9Spacecraft propulsive landings on unprepared regolith present in extra-terrestrial environments pose a high risk for space exploration missions. Plume/regolith interaction results in (1) the liberation of dust and debris particles that may collide with the landing vehicle and (2) craters whose shape itself can influence vehicle dynamics. To investigate such gas-granular interactions for large-scal ...
STTR Phase I 2018 National Aeronautics and Space Administration -
A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin
SBC: REACTION SYSTEMS, INC. Topic: T6Reducing 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