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.
-
Learning Algorithm Movement Predictor (LAMP) Module
SBC: BONN CORP. Topic: N/ABonn Corporation (BONN) has chosen to concentrate on researching a methodology that computes target movement prediction in real-time based on data fusion, data correlation, and learning algorithms, with the inhernt capability to accomodate user-definable inputs. BONN Will determine the required static (e.g., operational limitations and capabilities) and dynamic (e.g., weather and orders of ba ...
SBIR Phase I 1997 Department of DefenseNavy -
Common Flight Performance System (CFLIPS)
SBC: BONN CORP. Topic: N/ABONN has chosen to concentrate on an innovative concept that will lead to the design and development of a single, integrated flight performance model for various aircraft platforms. This flight performance model, to be known as the Common Flight Performance System CFLIPS), also features an easy-to-use interface that will enable TAMPS Mission Planning Module (MPM) developers to quickly and eas ...
SBIR Phase I 1997 Department of DefenseNavy -
Low-Leakage Brush Seals for Rocket Turbopumps
SBC: Concepts NREC, LLC Topic: N/AIt has been proven, for gas turbines, that brush seals exhibit substantially lower leakage in close clearance areas than conventional labyrinth seals. Direct efficiency gains from reducing seal leakage losses in turbopumps with brush seals potentially amounts to several percent of the total pump power consumption. As such, the case for transitioning brush seals to rocket turbopumps is compelling ...
SBIR Phase I 1997 Department of DefenseAir Force -
High Pressure Compressor Using an Axial-Flow, Mixed-Flow, and Centrifugal Stage with Interstage and Disc
SBC: Concepts NREC, LLC Topic: N/AHigh Pressure Compressor (HPC) pressure ratios of up to 40:1 are required to achieve 100:1 cycle pressure ratios. A multi-stage axial HPC configuration will be too long and heavy and too inefficient in later stages (at these higher pressure ratios). Increased tip clearance to span ratio will also lead to low efficiency and surge margin for the axial HPC. The innovations of the proposed work inc ...
SBIR Phase I 1997 Department of DefenseAir Force -
Compact, High Performance Compressor Diffusers for Small Gas Turbine Engines Requiring a Wide Operating Range
SBC: Concepts NREC, LLC Topic: N/ALow cost compact diffusers are needed for small gas turbine compressor stages to economically minimize centrifugal compressor overall diameter yet permit high efficiency and wide operating range. The proposer has performed over 130 different detailed tests (on more than 40 different stage configurations) with various conventional and novel diffusers (vaneless, low solidity airfoil, channel, tande ...
SBIR Phase I 1997 Department of DefenseArmy -
System for Detection, Measurement, and Avoidance of High Cycle Fatigue in Turbine Engines
SBC: Concepts NREC, LLC Topic: N/AHigh cycle fatigue of turbine engines is of vital concern to the Navy. The proposed project applies an innovative measurement system for blade vibration to an engine health monitoring (EHM) system for monitoring and avoiding HCF damage in turbine engine fans and compressors. Although technical feasibility of the instrumentation system was shown under a prior Phase I Army SBIR, operational f ...
SBIR Phase I 1997 Department of DefenseNavy -
Impulse Feedback-Based Health Management System For Aircraft Engine Systems
SBC: Concepts NREC, LLC Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
SBIR Phase I: Modern Design and Engineering Education in theAgile Engineering World
SBC: Concepts NREC, LLC Topic: N/AN/A
SBIR Phase I 1997 National Science Foundation -
Integrated Turbopump Design System For Improved Performance And Reduced Cost
SBC: Concepts NREC, LLC Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
Rocket Engine Analysis Codes on the Internet
SBC: Curtis Johnson Topic: N/AWe propose starting a commercial Internet website that will provide access to a variety of computer codes for the purpose of analyzing rocket engines and rocket engine components. Users will be able to execute well-maintained computer codes over the Internet. The codes found on the website will be an improvement on what is currently available since they will be maintained and upgraded by a conso ...
SBIR Phase I 1997 Department of DefenseAir Force