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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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The Cryogenic Impact Resistant Evaluation of Composite Materials for Use in Composite Pressure Vessels with an Additional Cryogenic Bonding Scope
SBC: HYPERCOMP ENGINEERING INC Topic: T801The intent of the proposed effort is to investigate the detailed composite material performance characteristics after being subjected to cryogenic temperatures and impact damage. HyPerComp Engineering, Inc. (HEI) and Utah State University (USU) further propose to correlate these characteristics to composite overwrapped pressure vessels (COPVs) and demonstrate the correlation through actual COPV t ...
STTR Phase II 2007 National Aeronautics and Space Administration -
Plume Diagnostics for Combustion Stability
SBC: SIERRA ENGINEERING, INC. Topic: T901Sierra Engineering Inc. and Purdue University propose to develop a non-intrusive plume instrument capable of detecting and diagnosing combustion instability. This Stability Diagnostic System (SDS) will be designed, assembled, and tested during this effort. The SDS will include a high-speed video camera and multiple photodiode detectors for observing the plume. It will also include a software pa ...
STTR Phase II 2007 National Aeronautics and Space Administration -
Defining the coupled effects of cryogenic, space-radiation, and hypervelocity impact damamge on COPV's
SBC: HYPERCOMP ENGINEERING INC Topic: X303The intent of the proposed effort is to investigate the detailed composite overwrapped pressure vessel (COPV) performance characteristics after being subject to irradiation, hypervelocity micro-meteor impact, and cryogenic environments. This will result in a safer, more reliable design for high performance COPVs. This intent will be achieved via empirical characterization of composite raw materia ...
SBIR Phase II 2007 National Aeronautics and Space Administration -
Integrated Variable-Fidelity Tool Set For Modeling and Simulation of Aeroservothermoelasticity-Propulsion (ASTE-P) Effects For Aerospace Vehicles Ranging From Subsonic to Hypersonic Flight
SBC: Advanced Dynamics, Inc. Topic: A204The proposed research program aims at developing a variable-fidelity software tool set for aeroservothermoelastic-propulsive (ASTE-P) modeling that can be routinely applied to the design of aerospace vehicles. The tool set can be applied to conventional vehicle types as well as hypersonic vehicles. The major issues involved in ASTE-P modeling and simulation will be significantly and extensively in ...
SBIR Phase I 2007 National Aeronautics and Space Administration -
Graphic Displays to Facilitate Rapid Discovery, Diagnosis and Treatment of Medical Emergencies
SBC: Axon Medical Inc Topic: N/AThis project develops a display for visually representing physiologic data, to enhance a non-physician astronaut's ability to assess, comprehend and rapidly stabilize an injured crewmember's vital signs. With longer duration missions further from earth involving more dangerous activities, the need for more autonomous emergency medical care becomes acute Our prior research has shown that graphic di ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
Better Pressure Vessel Impact Resistance Utilizing Filament Wound Hybrid Fibers.
SBC: HYPERCOMP ENGINEERING INC Topic: N/AHyPerComp Engineering, Inc. proposes to develop filament wound composite pressure vessels with superior low and high velocity impact resistance as well as improved high temperature (fire) survivability. The current generation of high performance filament wound composite pressure vessels as utilized in solid propellant propulsion, space craft energy storage systems, launch tubes, self contained bre ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
Better Pressure Vessel Impact Resistance Utilizing Filament Wound Hybrid Fibers.
SBC: HYPERCOMP ENGINEERING INC Topic: N/AHyPerComp Engineering, Inc. proposes to develop filament wound composite pressure vessels with superior low and high velocity impact resistance as well as improved high temperature (fire) survivability. The current generation of high performance filament wound composite pressure vessels as utilized in solid propellant propulsion, space craft energy storage systems, launch tubes, self contained bre ...
SBIR Phase II 2002 National Aeronautics and Space Administration -
Shared Aperture Diffractive Optical Elements for LIDAR Reception
SBC: Ralcon Dev Lab Topic: N/AConical scanning LIDAR systems and laser ranging systems that measure atmospheric backscatter, clouds, aerosols, winds, trace species, and sub-surface ocean layers require ruggedized construction and easy alignment. We are proposing to reduce the complexity and alignment chores by building five telescope objectives into one large shared aperture using holographic volume multiplexing techniques sim ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
Shared Aperture Diffractive Optical Elements for LIDAR Reception
SBC: Ralcon Dev Lab Topic: N/AConical scanning LIDAR systems and laser ranging systems that measure atmospheric backscatter, clouds, aerosols, winds, trace species, and sub-surface ocean layers require ruggedized construction and easy alignment. We are proposing to reduce the complexity and alignment chores by building five telescope objectives into one large shared aperture using holographic volume multiplexing techniques sim ...
SBIR Phase II 2002 National Aeronautics and Space Administration -
An Innovative Method of NOX Reduction Through Fuel Additives for the UEET Program
SBC: Software And Engineering Associates, Inc. Topic: N/AThe opportunity addressed in this proposal is to transfer a fuel-additive technology developed for NOx and particulate matter reduction in diesel fuels, to applications in ultra-efficient jet engine fuels, with no reduction in performance and power output of the engine. The innovation is based on a novel fuel additive, PuriNOx(TM), developed by Lubrizol Corporation. Unlike conventional fuel additi ...
SBIR Phase I 2002 National Aeronautics and Space Administration