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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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Hybrid Guidance System for Relative Navigation
SBC: Advanced Optical Systems, Inc Topic: S801Automated Rendezvous and Capture (AR&C) is a critical United States technology gap. AR&C is identified as a critical enabling technology for future NASA Exploration and DoD missions including NASA's CEV, operation and commercial cargo re-supply to ISS, lunar transfer vehicle assembly and MARS missions. Multiple sensors that provide relative measurements of range, bearing and pose are the key to me ...
SBIR Phase II 2007 National Aeronautics and Space Administration -
Development of a Database Management System to Enable Rapid, Efficient Assay Design for Use in Detection and Diagnosis of Human Exposure to Biological
SBC: CFD RESEARCH CORPORATION Topic: CBD07114The primary objective of this effort is to design and develop a database management system (DBMS) and enable the integrated interpretation of the vast amounts of genomic and proteomic data in proper biological context. This DBMS will enable the development of diagnostic assays for human exposure to specific biological threat agents using an existing suite of systems biology tools. The DBMS design ...
SBIR Phase I 2007 Department of DefenseOffice for Chemical and Biological Defense -
Improved Models and Tools for Prediction of Radiation Effects on Space Electronics in Wide Temperature Range
SBC: CFD RESEARCH CORPORATION Topic: X204All NASA exploration systems operate in the extreme environments of space (Moon, Mars, etc.) and require reliable electronics capable of handling a wide temperature range (-180ºC to +130ºC) and high radiation levels. To design low-temperature radiation-hardened (rad-hard) electronics and predict circuit and system characteristics, such as error rates, modeling tools are required at multiple leve ...
SBIR Phase I 2007 National Aeronautics and Space Administration -
Novel Solar Cell Nanotechnology for Improved Efficiency and Radiation Hardness
SBC: CFD RESEARCH CORPORATION Topic: X301Significant improvements in photovoltaic materials and systems are required to enable NASA future exploration missions. In this project, CFD Research Corporation (CFDRC) with University of California Riverside (UCR), Rochester Institute of Technology, and International Photonics will: 1) develop and provide reliable, validated computational tools for assessment, design, and optimization of novel ...
SBIR Phase II 2007 National Aeronautics and Space Administration -
Non-Destructive Detection and Separation of Radiation Damaged Cells in Miniaturized, Inexpensive Device
SBC: CFD RESEARCH CORPORATION Topic: T102There is a clear and well-identified need for rapid, efficient, non-destructive detection and isolation of radiation damaged cells. Available commercial technologies are expensive, require core facilities and use destructive methods. We propose to develop and demonstrate a novel fully automated, microfluidics-based device for identification and sorting of radiation damaged cells. The final produc ...
STTR Phase I 2007 National Aeronautics and Space Administration -
Numerical Simulation of Rocket Exhaust Interaction with Lunar Soil
SBC: CFD RESEARCH CORPORATION Topic: T602Rocket plume impingement may cause significant damage and contaminate co-landed spacecraft and surrounding habitat structures during Lunar landing operations. Under this proposed SBIR program, CFDRC and the University of Florida will develop an innovative high-fidelity simulation system for predicting surface erosion and debris transport caused by rocket plume impingement on lunar surface. This si ...
STTR Phase I 2007 National Aeronautics and Space Administration -
Advanced Nongray Radiation Module in the LOCI Framework for Combustion CFD
SBC: CFD RESEARCH CORPORATION Topic: T802Radiative heat fluxes are important in the design of launch vehicles for Project Constellation. In this Phase II STTR, CFDRC and its partner Mississippi State University will develop an innovative, comprehensive, high fidelity radiation module in the LOCI CFD framework that will enable NASA to design/analyze heat transfer challenges that include radiation. In Phase I, CFDRC/MSU successfully demo ...
STTR Phase II 2007 National Aeronautics and Space Administration -
Computational Tool for Aerothermal Environment Around Transatmospheric Vehicles
SBC: CFD RESEARCH CORPORATION Topic: A206The goal of this Project is to develop a high-fidelity computational tool for accurate prediction of aerothermal environment on transatmospheric vehicles. This computational tool will be based on the Unified Flow Solver (UFS) developed at CFDRC for hybrid simulations of rarefied, transitional and continuum flows. In this Project, the UFS will be enhanced with advanced non-equilibrium chemistry cou ...
SBIR Phase I 2007 National Aeronautics and Space Administration -
Multi-Physics Computational Modeling Tool for Materials Damage Assessment
SBC: DIGITAL FUSION SOLUTIONS, INC. Topic: A201The innovation proposed here is to provide a multi-physics modeling tool for materials damage assessment for application to future aircraft design. The software compute engine is based on an existing state-of-art multi-physics solver using first principles of mechanical engineering. Phase I will solve two significant NASA cases using this solver: 1) Coupled fluid-structure simulation of an aircr ...
SBIR Phase I 2007 National Aeronautics and Space Administration -
Oxygen-Methane Thruster
SBC: Orion Propulsion, Inc. Topic: X701Two main innovations will be developed in the Phase II effort that are fundamentally associated with our gaseous oxygen/gaseous methane RCS thruster. The first innovation is that of an integrated torch igniter/injector which, provides simple and reliable ignition for the thruster. The second innovation is the thruster's capability to operate with both gaseous and liquid propellants. This innova ...
SBIR Phase II 2007 National Aeronautics and Space Administration