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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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QMU in Integrated Spacecraft System Models
SBC: ACTA, LLC Topic: T5ACTA and Sandia National Laboratories propose to quantify and propagate substructure modeling uncertainty for reduced-order substructure models to higher levels of system assembly, thereby enabling predictive simulations of engineering designs with quantified margins and uncertainties for model-based flight qualification of complete spacecraft. A critical part of this process is the accurate mode ...
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 -
High-Fidelity Gas and Granular Flow Physics Models for Rocket Exhaust Interaction with Lunar Soil
SBC: CFD RESEARCH CORPORATION Topic: T701Current 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 -
Novel Real-Time Flight Envelope Monitoring System
SBC: ROLLING HILLS RESEARCH CORP Topic: T201The proposed innovation is an aircraft flight envelope monitoring system that will provide real-time in-cockpit estimations of aircraft flight envelope boundaries. The adaptable system will provide information on current and predicted aircraft performance and controllability, alerting the pilot to any aerodynamic degradation of the aircraft control surfaces. This includes heavy rain, in-flight i ...
STTR Phase II 2010 National Aeronautics and Space Administration -
A Reusable, Oxidizer-Cooled, Hybrid Aerospike Rocket Motor for Flight Test
SBC: ROLLING HILLS RESEARCH CORP Topic: T202The proposed innovation is to use the refrigerant capabilities of nitrous oxide (N2O) to provide the cooling required for reusable operation of an aerospike nozzle in conjunction with an N2O-HTPB (hydroxyl-terminated polybutadiene, a synthetic rubber that is used as a binder in solid rocket motors and as a fuel in hybrid rocket motors) hybrid rocket motor. The phase change cooling as liquid N2O i ...
STTR Phase II 2010 National Aeronautics and Space Administration -
Biotemplated Nano-Structured Materials for Advanced Li-ion Batteries
SBC: CFX BATTERY, INC. Topic: T301NASA has identified a critical need for pioneering advances in battery technology to give high performance, low-weight, durable and long-life power sources for future missions. In this Phase I proposal, CFX Battery, Inc. and Georgia Institute of Technology propose the chemical conversion of micron-sized, nano-structured templates available from renewable resources into functional electrode materia ...
STTR Phase I 2010 National Aeronautics and Space Administration -
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 -
Structural Health Monitoring with Fiber Bragg Grating and Piezo Arrays
SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP Topic: T201IFOS and its research institute collaborator, Washington State University (WSU), have demonstrated feasibility of a structural health monitoring (SHM) system for aerospace vehicles such as Unmanned Aerial Vehicles (UAVs) or commercial airliners. In Phase 1, a unique high-speed, high-channel count fiber Bragg grating (FBG) sensor interrogation system enabling a new Lamb wave-based damage detection ...
STTR Phase II 2010 National Aeronautics and Space Administration -
Highly Reliable Structural Health Monitoring of Smart Composite Vanes for Jet Engine
SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP Topic: T201Intelligent Fiber Optic Systems and Auburn University propose a Fiber Bragg Grating (FBG) integrated Structural Health Monitoring (SHM) sensor system capable of providing in-situ crack detection, location and quantification of damage, as well as validating structural models, using recent advances in non-contact, non-destructive dynamic testing of composite structures. The key innovation is an FBG- ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Thermal Stir Welding of High Strength and High Temperature Alloys for Aerospace Applications
SBC: Keystone Synergistic Enterprises, LLC Topic: T901The Keystone and MSU team propose to build on the successful feasibility demonstration conducted during Phase I to complete the development of solid-state joining of high strength and temperature alloys utilizing the Thermal Stir Welding process. The focus alloy for this project is Haynes 230; the alloy of choice typically utilized in rocket engine nozzel skirts. This class of alloy is difficult t ...
STTR Phase II 2010 National Aeronautics and Space Administration