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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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Numerical Simulation of Rocket Exhaust Interaction with Lunar Soil
SBC: CFD RESEARCH CORPORATION Topic: T602Rocket plume impingement can cause significant damage and contaminate co-landing spacecraft and surrounding habitat structures during lunar landing operations. CFDRC and the University of Florida will develop an innovative simulation system for predicting surface erosion and debris transport caused by lunar surface rocket plume impingement. This simulation system combines 1) a unified continuum-ra ...
STTR Phase II 2008 National Aeronautics and Space Administration -
Automation of Analysis Model Creation
SBC: Technosoft, Inc Topic: N06T018Although numerical analysis applications have proven to be effective and reasonably accurate, the effort required to develop the associated analysis models remains a challenging and time consuming task. While many meshing tools are currently available, decomposing and manipulating the design geometry and enhancing the topology for mesh construction are manual processes and place the heaviest dema ...
STTR Phase II 2008 Department of DefenseNavy -
An On-Chip Nano-Plasmonics Based Urine Protein Assay Cartridge
SBC: CFD RESEARCH CORPORATION Topic: T302Long-term exposure to microgravity and radiation during space exploration can pose a critical threat to the health of a flight crew. Real-time monitoring of urine protein levels is an effective way to follow the onset and progress of many diseases and guide the prompt selection of proper therapy. The success of such diagnostic tasks, which is strongly desired for flight missions, critically depend ...
STTR Phase I 2008 National Aeronautics and Space Administration -
Fuel/Oxidizer Injector Modeling in Sub- and Super-Critical Regimes for Deep Throttling Cryogenic Engines
SBC: CFD RESEARCH CORPORATION Topic: T802Accurate CFD modeling of fuel/oxidizer injection and combustion is needed to design and analyze liquid rocket engines. Currently, however, there is no mature modeling capability for liquid fuel/oxidizer injectors in LOCI-Chem, used by NASA and its contractors to analyze rocket engines. In this STTR, an innovative, high fidelity injection module will be developed that features the Level Set (LS) i ...
STTR Phase I 2008 National Aeronautics and Space Administration -
The Cyogenic Evaluation of Irradiated Composite Materials for Use in Composite Pressure Vessels
SBC: HYPERCOMP ENGINEERING INC Topic: T801HyPerComp Engineering, Inc. (HEI) proposes to continue the characterization of the cryogenic evaluation of irradiated composite materials for use in composite overwrap pressure vessels COPVs. The intent of the proposed effort is to study the constituent raw composite material properties that result from radiation exposure and tested at cryogenic temperatures. HEI and Mississippi State Universi ...
STTR Phase II 2006 National Aeronautics and Space Administration -
Advanced Nongray Radiation Module in the LOCI Framework for Combustion CFD
SBC: CFD RESEARCH CORPORATION Topic: T802In this STTR, an innovative, efficient and high fidelity computational tool to predict radiative heat transfer will be implemented in the LOCI framework. Radiative heat transfer in rocket engine combustion can play a significant role in determining engine performance and combustor wall heat loading. Radiation will also become increasingly important as hydrocarbon-based fuels are used in rocket pro ...
STTR Phase I 2006 National Aeronautics and Space Administration -
Assessment of Protective Properties of Optimized Flagellin Derivative Against Biologically Harmful Effects of Ionizing Irradiation During Space Flight
SBC: Cleveland Biolabs, Inc Topic: T102The goal of this proposal is to explore a novel proprietary biopharmaceutical agent, named deltaFL-AA', a first in the series of innovative radioprotectors to act as an agent providing protection of the organism against major space radiation risks. These risks include organism death resulting from acute irradiation as well as radiation-induced carcinogenesis caused by low-dose exposure. An unprece ...
STTR Phase I 2006 National Aeronautics and Space Administration -
The Cryogenic Impact Resistant Evaluation of Filament Wound Materials for Use in Composite Pressure Vessels
SBC: HYPERCOMP ENGINEERING INC Topic: T801HyPerComp Engineering Inc. (HEI) and Utah State University (USU) propose to develop technology for lightweight composite materials for use in composite structures suitable for both cryogenic and damage tolerant environments. The proposed effort will incorporate previous work performed by HEI in the cryogenic performance of composite materials as well as previously developed improved impact technol ...
STTR Phase I 2006 National Aeronautics and Space Administration -
Innovative Molybdenum Alloy for Extreme Operating Conditions
SBC: Plasma Processes, LLC Topic: T801Molybdenum has been identified as a promising material for many high temperature NASA applications due to its high melting temperature, resistance to liquid metals, resistance to hot hydrogen, high thermal conductivity, and relatively low density. However, molybdenum's ductile to brittle transition temperature is above room temperature, which makes fabricating complex components extremely difficu ...
STTR Phase I 2006 National Aeronautics and Space Administration -
Effect of Ambipolar Potential on the Propulsive Performance of the GDM Plasma Thruster
SBC: Reisz Engineers Topic: T801The gasdynamic mirror (GDM) plasma thruster has the ability to confine high-density plasma for the length of time required to heat it to the temperatures corresponding to specific impulse requirements. The often-cited plasma confinement time is directly proportional to the mirror ratio and the length, and is inversely proportional to the square root of ion energy. This confinement law, however, i ...
STTR Phase I 2004 National Aeronautics and Space Administration