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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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ADAPTIVE FOCAL-PLANE PROCESSOR FOR IMAGE ENHANCEMENT
SBC: Odetics Inc. Topic: N/ATHE PERFORMANCE OF IMAGING SYSTEMS IS HIGHLY DEPENDENT ON THE INTENSITY AND DISTRIBUTION OF LIGHT ILLUMINATING THE SCENE. THE HUMAN VISUAL SYSTEM PERFORMS WELL OVER A RANGE OF SCENE BRIGHTNESS FAR GREATER THAN THAT WHICH MAN-MADE IMAGE SENSING SYSTEMS ARE CAPABLE OF OPERATING. ODETICS, INC. PROPOSES AN OPTICAL MODEL WHICH: GREATLY INCREASES THERANGE AND VARIABILITY OF SCENE ILLUMINATION; VASTLY IM ...
SBIR Phase II 1987 National Aeronautics and Space Administration -
A DIGITAL PROCESSOR FOR AN EARTH HORIZON SENSOR ATTITUDE CONTROL SYSTEM
SBC: Ithaco, Inc. Topic: N/ATHIS IS A PROJECT LEADING TO DEFINITION OF A DIGITAL-PROCESSOR SYSTEM FOR SMALL SPACECRAFT. THE FIRST PHASE OF THE PROGRAM WILL EXAMINE SEVERAL SMALL-SATELLITE PROGRAMS TO DETERMINE A TYPICAL, SMALL-SATELLITE MISSION. NEXT, THESE REQUIREMENTS WILL BE TRANSLATED INTO SPECIFIC REQUIREMENTS FOR AN ATTITUDE-CONTROL SYSTEM THAT WILL GUIDE HARDWARE AND SOFTWARE DECISIONS. HARDWARE QUESTIONS AS INTERFACE ...
SBIR Phase II 1992 National Aeronautics and Space Administration -
A DIRECT CALORIMETRY SYSTEM WHEREBY METABOLIC HEAT RELEASES OF ANIMALS CAN BE MEASURED IN ORBITAL LABORATORIES
SBC: Geoscience Ltd Topic: N/AIF A PRACTICAL DIRECT CALORIMETER SYSTEM WERE AVAILABLE FOR THE MEASUREMENT OF METABOLIC HEAT RELEASES IN ANIMALS IN ORBITAL LABORATORIES, IT WOULD BE POSSIBLE TO QUANTIFY SUCH PROCESSES AS 1) CHANGES IN BONE MINERAL AND MUSCLE STATUS (AS A RESULT OF WEIGHTLESSNESS) AND 2) CHANGES IN THE IMMUNESYSTEM (AS A RESULT OF STRESS AND RADIATION FORCE FIELDS) INTERMS OF THE CORRESPONDING METABOLIC CHANGES. ...
SBIR Phase II 1987 National Aeronautics and Space Administration -
A DISTRIBUTED OBJECT-ORIENTED DATA FACILITY FOR LOCAL MEMORY PARALLEL COMPUTERS
SBC: Mimd Systems, Inc. Topic: N/ALOCAL MEMORY, PARALLEL PROCESSING COMPUTER SYSTEMS OFFER THE POTENTIAL TO REALIZE PREVIOUSLY UNAVAILABLE LEVELS OF PERFORMANCE AT COSTS FAR LOWER THAN CURRENT UNIPROCESSOR TECHNOLOGY PERMITS. HOWEVER, THE ARCHITECTURES OF THESE PARALLEL SYSTEMS PRESENT DIFFICULT PROBLEMS FOR BOTH DATA ACCESS AND DATA COMMUNICATIONS. THE ARACHNID SYSTEM IS PROPOSED AS A GENERAL SOLUTION TO THESE PROBLEMS. ARACHNID ...
SBIR Phase II 1992 National Aeronautics and Space Administration -
A 3-D Miniature LIDAR System for Mobile Robot Navigation
SBC: Honeybee Robotics, Ltd. Topic: X703Future lunar site operations will benefit from mobile robots, both autonomous and tele-operated, that complement or replace human extravehicular activity. Three-dimensional sensing technology is at the heart of such functionality, enabling reliable navigation in complex, dynamic environments, and serving as a valuable tool for inspection and site survey. Honeybee Robotics is therefore developing ...
SBIR Phase II 2009 National Aeronautics and Space Administration -
ADVANCED ON-CHIP DIVIDER FOR MONOLITHIC MICROWAVE VCOS
SBC: Microwave Monolithics Inc. Topic: N/ADEVELOPMENT OF AN ADVANCED MONOLITHIC GAAS 8.5 VOLTAGE CONTROLLED OSCILLATOR WITH ON-CHIP GENERATION OF A LOW FREQUENCY REFERENCE OUTPUT, SUITABLE FOR PHASE LOCKED LOOP APPLICATIONS, IS PROPOSED. CIRCUIT ELEMENTS AND DESIGNS TECHNIQUES TRADITIONALLY RESERVED FOR MICROWAVE APPLICATIONSARE UTILIZED TO OBTAIN THE HIGH SPEED DIVIDE BY N CIRCUIT. A COHERENT REFERENCE SIGNAL IN THE 90-200 MHZ RANGE IS T ...
SBIR Phase II 1987 National Aeronautics and Space Administration -
ADVANCED POWDER METALLURGY TECHNIQUES TO MANUFACTURE HIGH STRENGTH REFRACTORY METAL FIBERS
SBC: Metadyne Inc. Topic: N/AMANUFACTURING METHOD FOR HIGH ELEVATED-TEMPERATURE STRENGTH FIBERS INCORPORATING RECENT ADVANCES IN SINTERING TECHNOLOGYAND REFRACTORY METAL ALLOY DEVELOPMENT WILL BE INVESTIGATED.A CONTROLLED ATMOSPHERE SINTERING OF POWDER METALLURGY INGOTS OF NEW MOLYBDENUM AND TUNGSTEN ALLOYS UNDER A SELECTED CHEMICAL POTENTIAL ENVIRONMENT, IN CONJUCTION WITH SUBSEQUENT OPTIMIZED WIRE DRAWING PROCESS MAY PRODUC ...
SBIR Phase II 1987 National Aeronautics and Space Administration -
Advanced Technologies for Discrete-Parts Manufacturing
SBC: MATERIALS INNOVATION TECHNOLOGIES, LLC Topic: DLA07001Materials Innovation Technologies LLC is developing a method for making polymer matrix composites fiber preforms that has the potential to revolutionize the industry. The Three Dimensional Engineered Preform (3-DEP) process represents the state-of-the art in chopped fiber preform manufacture. 3-DEP produces a homogeneous fiber distribution within parts and consistent part weight and dimensions f ...
SBIR Phase II 2009 Department of DefenseDefense Logistics Agency -
AERODYNAMIC CONTROL OF AIRCRAFT USING MINIATURE ROTATABLE NOSE-BOOM STRAKES
SBC: ROLLING HILLS RESEARCH CORP Topic: N/ATHE GOAL OF THIS PROJECT IS AN INNOVATIVE METHOD OF ENHANCING THE CONTROLLABILITY OF AIRCRAFT AT MODERATE-TO-HIGH ANGLES-OF-ATTACK (AOA) BY CONTROLLING THE FOREBODY VORTEX FLOW WITH ROTATABLE NOSE-BOOM STRAKES. THE IDEA IS TO CONTROL THE ASYMMETRY OF THE NOSE-BOOM WAKE BY PLACING SMALL, MOVABLE STRAKES ON THE NOSE-BOOM. THE WAKE THEN ACTS AS A CONTROLLED PERTURBATION ON THE FOREBODY FLOW AND SUBSE ...
SBIR Phase II 1992 National Aeronautics and Space Administration -
Aeroelastic Uncertainty Analysis Toolbox
SBC: Systems Technology, Inc. Topic: A204Flutter is a potentially explosive phenomenon that results from the simultaneous interaction of aerodynamic, structural, and inertial forces. The nature of flutter mandates that flight testing be cautious and conservative. In addition to the flutter instability, adverse aeroelastic phenomena include limit cycle oscillations, buffeting, buzz, and undesirable gust response. The analytical prediction ...
SBIR Phase II 2009 National Aeronautics and Space Administration