GoHypersonic Inc.

Basic Information

714 E. Monument Ave
Suite 119
Dayton, OH, 45402-1382

http://www.gohypersonic.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 780026220
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 16


  1. Non-Linear Damage Model for Carbon-Carbon Composite Design

    Amount: $79,977.00

    Currently, difficulties in modeling non-linear behavior and damage modes of carbon-carbon (C/C) composites beyond simplified in-plane models prevent accurate assessment of bending load and thermal str ...

    SBIR Phase I 2014 Navy Department of Defense
  2. Reentry Vehicle and Wake Analysis Tool

    Amount: $1,596,296.00

    During hypersonic reentry, the flow around reentry vehicles is ionized resulting in electro-optical and infrared emissions, detectable radar cross-sections, and attenuation of signals transmitted thro ...

    SBIR Phase II 2012 Department of Defense Missile Defense Agency
  3. Advanced Reentry Vehicle and Wake Models

    Amount: $100,000.00

    At hypersonic flow conditions, the flow field around reentry vehicles is ionized, resulting in electro-optical emissions, detectable radar cross-sections, and attenuation of signals transmitted throug ...

    SBIR Phase I 2011 Department of Defense Missile Defense Agency
  4. Advanced Analysis and Design Tool for Scramjet Air-frame Propulsion Integration

    Amount: $149,988.00

    ABSTRACT: This SBIR program provides the GHI team with the opportunity to integrate state-of-the-art Computational Fluid Dynamics (CFD) codes into a scramjet engine analysis tool that will enable the ...

    SBIR Phase I 2011 Department of Defense Air Force
  5. Flight-Capable Self-Starting Scramjet Inlets

    Amount: $749,979.00

    ABSTRACT: GoHypersonic Inc. is proud to present the following Phase II SBIR Proposal to the AFRL/RZA involving the development, fabrication, and testing of a high-performing flight-capable self-start ...

    SBIR Phase II 2011 Department of Defense Air Force
  6. Flight-Capable Self-Starting Scramjet Inlets

    Amount: $99,990.00

    The proposed Phase I SBIR seeks to develop passive self-starting inlet technologies and extend inlet operability to a range of at least 3 Mach numbers. This development will be completed using GHI’s ...

    SBIR Phase I 2010 Air Force Department of Defense
  7. Innovative Aerodynamic Measurement for Integrated Hypersonic Inlets

    Amount: $99,993.00

    This SBIR gives GHI the chance to evolve our measurement techniques within our overarching design-to-test process. If we can develop rapid instrumentation design methods and techniques that can enabl ...

    SBIR Phase I 2010 Air Force Department of Defense
  8. Combined Cycle Propulsion Integration

    Amount: $649,986.00

    The two main objectives of this proposal are to refine the combined cycle engine capabilities in GHIs design tool, Eco, and to flight test a combined cycle powered vehicle concept designed for flight ...

    SBIR Phase II 2010 Department of Defense Air Force
  9. Hypersonic Propulsion-Airframe Integration

    Amount: $99,993.00

    This SBIR presents an opportunity to study alternate scramjet engine configurations in an effort to increase spillage to levels between inward-turning and planar inlets while understanding the impact ...

    SBIR Phase I 2008 Air Force Department of Defense
  10. Combined Cycle Propulsion Integration

    Amount: $99,986.00

    The work proposed here provides an opportunity to take what we have learned within the DARPA Falcon program on TBCC inlet design and our current AF RBCC/TBCC nozzle research and integrate them into ou ...

    SBIR Phase I 2008 Air Force Department of Defense

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