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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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Materials and Structures Optimization / Process Development for the Mega-ROSA / ROSA Solar Array
SBC: Deployable Space Systems, Inc. Topic: T301Deployable Space Systems, Inc. (DSS), in collaboration with the University of California, Santa Barbara (UCSB), Department of Mechanical Engineering, will focus the proposed NASA STTR Phase 2 program on the materials optimization, structures optimization, creep / relaxation phenomena characterization and analytical modeling, and manufacturing process optimization/development for the Mega-ROSA/ROSA ...
STTR Phase II 2013 National Aeronautics and Space Administration -
Hybrid Propulsion for Upper-Stage Boosters
SBC: EXQUADRUM INC Topic: T201The objective of the proposed research and development effort is to demonstrate the feasibility of an innovative approach to high-performance hybrid propulsion for upper-stages. The missions for these propulsion systems include launching small- and nano-satellites and conducting hypersonic flight test operations. The focus of the research effort will be on achieving high specific impulse by mean ...
STTR Phase II 2013 National Aeronautics and Space Administration -
=Miniaurizable, High Performance, Fiber-Optic Gyroscopes for Small Satellites
SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP Topic: T401This Phase 2 program builds on a successful Phase 1 effort that demonstrated practical engineering methods as well as continuing development paths to build smaller high performance gyro systems suitable for small satellite applications. This program will execute a logical follow-on endeavor by (a) using existing components that satisfy the specifications matrix, and (b) developing new components ...
STTR Phase II 2013 National Aeronautics and Space Administration -
A Self-Regulating Freezable Heat Exchanger for Spacecraft
SBC: TDA RESEARCH, INC. Topic: T601A spacecraft thermal control system must keep the vehicle, avionics and atmosphere (if crewed) within a defined temperature range. Since water is non-toxic and good for heat transport, it is typically used as the coolant that circulates within the crew cabin boundary. This loop then interfaces with another low freeze point fluid, such as ammonia, for transport of heat to a radiator where the tempe ...
STTR Phase II 2013 National Aeronautics and Space Administration -
Lab-on-a-Robot Platform for In-Situ Planetary Compositional Analysis
SBC: HJ SCIENCE & TECHNOLOGY INC Topic: T501This joint STTR research effort between HJ Science & Technology and the University of Texas at San Antonio seeks to establish a highly integrated mobile "lab-on-a-chip" platform next generation "lab-on-a-robot" (LOAR) - capable of in-situ, high throughput, and simultaneous identification and characterization of universal classes of ions, molecules, and biomolecules for NASA in-situ planetary co ...
STTR Phase II 2013 National Aeronautics and Space Administration -
Modular Electric Propulsion Test Bed Aircraft
SBC: ROLLING HILLS RESEARCH CORP Topic: T901A hybrid electric aircraft simulation system and test bed is proposed to provide a dedicated development environment for the rigorous study and advancement of hybrid electric powered aircraft. The new test bed and simulation system will provide a dedicated platform and set of analysis tools to study, design, and test hybrid electric powered propulsion components and systems for use in commercial, ...
STTR Phase II 2014 National Aeronautics and Space Administration -
Attitude Control Enhancement Using Distributed Wing Load Sensing for Dynamic Servoelastic Control
SBC: Systems Technology, Inc. Topic: T402Strain sensor information is used in nature to achieve robust flight, good rejection of wind disturbances, and stable head motion. Similar man-made sensing devices will be used to demonstrate flight control using Fly-by-Feel, with the overall objective of achieving similarly good performance with piloted and autonomous vehicles. The Phase I work demonstrated the feasibility of using strain sensor ...
STTR Phase II 2014 National Aeronautics and Space Administration -
Radiation Hard Monolithic SDRAM to Support DDR2 and DDR3 Architectures
SBC: Space Micro Inc. Topic: T1501Space Micro has developed the architecture for a radiation hardened memory subsystem that targets DDR3-and-beyond generations of DRAM. The architecture combines server platform error correction and memory buffer-on-board schemes with Space Micro proprietary techniques for radiation hardening and size, weight, and power reduction. During the NASA Phase I effort, Space Micro demonstrated two key ele ...
STTR Phase II 2014 National Aeronautics and Space Administration -
Particle Flow Physics Modeling for Extreme Environments
SBC: CFD RESEARCH CORPORATION Topic: T403The liberation of particles induced by rocket plume flow from spacecraft landing on unprepared regolith of the Moon, Mars, and other destinations poses high mission risks for robotic and human exploration activities. This process occurs in a combination of "extreme environments" that combine low gravity, little or no atmosphere, rocket exhaust gas flow that is supersonic and partially rarefied, an ...
STTR Phase II 2014 National Aeronautics and Space Administration -
High-Fidelity Prediction of Launch Vehicle Lift-off Acoustic Environment
SBC: CFD RESEARCH CORPORATION Topic: T101Launch vehicles experience extreme acoustic loads during liftoff driven by the interaction of rocket plumes and plume-generated acoustic waves with ground structures. Currently employed predictive capabilities are too dissipative to accurately resolve the propagation of waves throughout the launch environment. Higher fidelity non-dissipative analysis tools are critically needed to design mitigatio ...
STTR Phase II 2014 National Aeronautics and Space Administration