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Award Data

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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.

  1. Automated Fiber Placement of Thin-Ply Composite Materials for Large Aerospace Structures

    SBC: NEXTGEN MATERIALS & PROCESSING LLC            Topic: T12

    Leveraging their prior experience working with automated fiber placement (AFP) of thin-ply composite materials, NextGen Materials & Processing LLC and the University of Massachusetts Lowell will utilize a Design of Experiments approach, combined with analytical modeling, to identify the critical material, slitting, spooling, and AFP parameters that influence the repeatable, high quality laydown of ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  2. Coordination of Heterogeneous Robot Swarms for Planetary Logistics Operations

    SBC: VECNA TECHNOLOGIES, INC            Topic: T4

    Swarm robotics is one of the key enabling technologies for significantly extending mankind's reach beyond the Earth's surface. However, when bringing theory to practice, challenging problems related to the coordination and control of these swarms quickly arise. Vecna Robotics proposes a collaboration with MIT to extend existing autonomy behaviors and test platforms to address a class of pl ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  3. Efficient CO2 and H2O Removal with Novel Adsorbentsfor Life Support Applications on Mars

    SBC: MOSAIC MATERIALS, INC.            Topic: T6

    Very low CO2 concentrations that accumulate quickly from human respiration can have dramatic health effects, and thus in NASA’s history many technical removal strategies for CO2 from a confined atmosphere have been suggested and explored. A CO2 removal system that functions in a is a new area of research, as the primary CO2 removal component in the state-of-the-art system doesn’t have the adso ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  4. A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin

    SBC: REACTION SYSTEMS, INC.            Topic: T6

    Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal assembly (CDRA). While it has performed well on the ISS, managers have concluded that using the device to reach the new ppCO2 limit of 2.0 mm Hg is not practical and a new method is needed.In this projec ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  5. Integrated Photonic Filters for RF Signal Processing

    SBC: OEWAVES, INC            Topic: T8

    In this Project, OEwaves Inc. and Georgia Tech team propose to research and develop a unique RF photonic receiver front-end enabling microwave signal processing at a heterogeneously integrated photonic platform. In particular, we propose to develop a new technology for photonic microwave filters based on the new advances in Si-based integrated photonics. We will exploit the expertise of the team m ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  6. Regeneratively Cooled Ceramic Matrix Composite Nozzle Assembly for Reduced Weight

    SBC: PHYSICAL SCIENCES INC.            Topic: T9

    All rocket missions benefit from having lower structural mass and higher specific impulse, both of which contribute to larger payload fractions and therefore lower mission cost. High temperature materials such as ceramic matrix composites (CMCs) are an avenue to lower engine mass because of the low density and high specific strength of the material. They also have a high maximum temperature and so ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  7. Nanosat Maneuvering and Orbital Transfer Stage

    SBC: PARABILIS SPACE TECHNOLOGIES INC            Topic: T1

    The proposed innovation is a modular, high-performance orbital transfer stage (OTS) vehicle for Nanosats and Microsats launched as secondary payloads and require maneuvering to their desired orbits. The OTS has a modular design, and can accommodate payloads ranging from 5kg 3U size Nanosats to >50kg Microsat size vehicles. The propulsion system uses hydroxyl-terminated polybutadiene (HTPB) fuel wi ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  8. Aeroservoelastic Multifidelity Design of Biomimetic Aircraft (AMuBA)

    SBC: Intelligent Automation, Inc.            Topic: T15

    NASA has been investigating morphing aircraft for multi-mission capabilities and performance improvements in existing fixed-wing aircraft. In addition, the design of aeroelastic aircraft that can control the structural flexibility to their advantage, is an open area of research and development. In spite of the plethora of work on morphing aircraft and long slender wings, the goal of fielding such ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  9. Additive Manufacture of Refractory Metal Propulsion Components

    SBC: GEOPLASMA LLC            Topic: T9

    Niobium alloy (C-103) reaction control system (RCS) chambers have been used on numerous NASA programs. However at elevated temperatures, the strength of C-103 decreases significantly. Higher strength niobium alloys have been developed, but these alloys lack the formability of C-103. Recently, Additive Manufacture (AM) of niobium and C-103 has been demonstrated using powder bed electron beam me ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  10. Refractory Additively Manufactured Affordable Launch Vehicle RCS

    SBC: VALLEY TECH SYSTEMS INC            Topic: T1

    Due to the rapid maturity of small satellite technologies to meet near term commercial, science and military space applications there is a driving need for development of increased affordable space launch system capability. To address this need, Valley Tech Systems and the University of Texas El Paso (UTEP) is proposing evolving our innovative Affordable Launch Vehicle Reaction Control System (AL ...

    STTR Phase I 2018 National Aeronautics and Space Administration
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