You are here
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.
-
ADVANCED ACCELERATORS BASED ON SUPERCONDUCTING BAND GAP STRUCTURES
SBC: Accsys Technology, Inc. Topic: N/ATHIS PROJECT INVESTIGATES A NEW TYPE OF HIGH Q RESONANT STRUCTURE, WHICH HAS RECENTLY BEEN DEMONSTRATED, TO DEVELOP HIGH GRADIENT, SUPERCONDUCTING ACCELERATOR CAVITIES. BASED ON THE CONCEPT OF A PHOTONIC BAND GAP (PBG) RESONATOR, THESE NEW STRUCTURES ARE PHYSICALLY SIGNIFICANTLY DIFFERENT FROM THE RESONANT CAVITIES CURRENTLY USED IN NORMAL SUPERCONDUCTING DEVICES. A RESONANT MODE SUITABLE FOR ACCE ...
SBIR Phase II 1993 Department of Energy -
AN EXTENDED INTERDIGITAL NIOBIUM SUPERCONDUCTING LINAC STRUCTURE FOR LOW VELOCITY HEAVY IONS
SBC: Accsys Technology, Inc. Topic: N/ATHE USE OF THE RADIO FREQUENCY SUPERCONDUCTING ION LINACS HAS GROWN STEADILY OVER THE PAST 15 YEARS, PRIMARILY FOR APPLICATIONS IN NUCLEAR AND ATOMIC PHYSICS WHERE FLEXIBILITY N ION SPECIES AND ENERGY ARE REQUIRED. THIS TECHNOLOGY CONTINUES TO BE ACTIVELY DEVELOPED AT SEVERAL LABORATORIES WORLDWIDE. A RECENT DEVELOPMENT AT THE ARGONNE TANDEM LINAC ACCELERATOR SYSTEM (ATLAS) FOR THE NEW POSITIVE IO ...
SBIR Phase I 1993 Department of Energy -
A Variable Thurst Detonation Wave Engine, DWE, for Mach 0 to 3 Applications
SBC: Advanced Projects Research, Incorporated Topic: N/AThis proposal describes a novel, high thrust density Detonation Wave Engine (DWE) applicable to the Mach range of 0 to 3. The geometry of this novel engine concept naturally provides for integration into a new Combined Cycle Engine with Ramjets. The concept is an intermittent combustion jet engine that harnesses travelling detonation waves to accomplish compression and chemical reaction. The goal ...
SBIR Phase I 1993 Department of DefenseAir Force -
A Variable Thrust Detonation Wave Engine DWE for Mach 0 to 3
SBC: Advanced Projects Research, Incorporated Topic: N/AAn innovative actively cooled structure concept is proposed which integrates proven cooling techniques and state-of-the-art fabrication methods to extend the maximum combustor wall temperature, thereby reducing cooling requirements and aircraft weight while improving engine performance. Specifically, CONvective and TRANspiration cooling (CONTRAN) are uniquely combined, relying on hydrogen coolant ...
SBIR Phase I 1993 Department of DefenseAir Force -
Hy-Scram: An Oblique Detonation Wave Hypervelocity Scramjet Engine
SBC: Advanced Projects Research, Incorporated Topic: N/AN/A
SBIR Phase I 1993 Department of DefenseAir Force -
A WAVELENGTH DISPERSIVE SPECTROMETER FOR ANALYTICAL ELECTRON MICROSCOPY
SBC: Aracor Topic: N/ATHE DEVELOPMENT OF A NOVEL NON-SCANNING WAVELENGTH DISPERSIVE SPECROMETER (WDS) FOR ANALYTICAL ELECTRON MICROSCOPY (AEM) IS THE OBJECTIVE OF THIS PROJECT. THIS SPECTROMETER IS DESIGNED TO PROVIDE SUFFICIENT ENERGY RESOLUTION OVER BROAD REGIONS OF THE SOFT X-RAY SPECTRAL REGION (FROM 100 TO 2000 EV) TO ALLOW THE OBSERVATION OF THE K-EMISSIONS OF THE LIGHT ELEMENTS (THOSSE WITH ATOMIC NUMBERS LESS T ...
SBIR Phase I 1993 Department of Energy -
MONOLITHICALLY INTEGRATED DETECTOR ARRAYS
SBC: Aracor Topic: N/ATHIS PHASE I PROJECT WILL DEVELOP A DETECTOR TECHNOLOGY FOR TRACKING PARTICLES CLOSE TO THE BEAM PIPE IN NEW GENERATION ACCELERATOR EXPERIMENTS. HIGH SPATIAL RESOLUTION, HIGH SPEED DATA READOUT, COMPACT SIZE, LOW POWER, AND RADIATION HARDNESS WILL BE ACHIEVED BY INCORPORATING A HIGH RESISTIVITY, DETECTOR GRADE, 300 MUM THICK WAFER PATTERNED WITH P(+) DETECTOR ELEMENTS INTO THE RADIATION HARDENED, ...
SBIR Phase I 1993 Department of Energy -
Instrumentation for Non-Intrusive Water Droplet Size and Mass Flux Measurements Utilizing the Phase Doppler Method
SBC: Aerometrics Inc. Topic: N/AThere is a need for non-intrusive instrumentation to characterize the drop size distribution and volume flux in support of on-line engine/inlet icing tests. The ducts may vary from three to twelve feet in diameter with flow field speeds from Mach 0.2 to 0.5. The Phase Doppler technique offers the best potential for making these measurements non-intrusively and with sufficient accuracy to meet the ...
SBIR Phase I 1993 Department of DefenseAir Force -
Characterization of Simulated Weather Environments In Aerospace Ground Test Cells.
SBC: Aerometrics Inc. Topic: N/AN/A
SBIR Phase I 1993 Department of DefenseAir Force -
INFLATABLE SMART MISSILE WING DESIGN EVALUATION
SBC: AEROTECH ENGINEERING & RESEARCH CORP. Topic: N/ATHREE AREAS OF ACTIVE MISSILE WING RESEARCH WILL BE PURSUED. THE FIRST SECTION WILL EVALUATE THE MATERIALS TO BE USED IN THE INFLATABLE WING SPARS, RIBS, SKINS, PRESSURE BLADDERS AND ACTIVE ELEMENTS. SPECIMENS OF HIGH ORTHOGONALITY COMPOSITES (POLYURETHANE-GRAPHITE) WILL BE CONSTRUCTED ALONG WITH SAMPLE ISOTROPIC BLADDER MATERIALS (MYLAR OR TEFLON) SO THAT THEIR FUNDAMENTAL PROPERTIES CAN BE EVALU ...
SBIR Phase II 1993 Department of DefenseAir Force