Gohypersonic, Inc.

714 E. Monument Ave Suite 19
Dayton, OH 45402
http://www.gohypersonic.com
16 Employees

SBIR Award Summary

Total Number of Awards 12
Total Value of Awards $4.98MM
First Award Date 08/07/06
Most Recent Award Date 05/23/14

Key Personnel

Last Name Name Awards Contact
Jacobsen Dr. Lance Jacobsen 9 Message
Drayna Travis Drayna 2 Message
Gaston Zachary Gaston 1 Message

12 Awards Won

Phase 1 SBIR

Agency: Navy
Topic: N141-082
Budget: 05/23/14 - 11/24/14

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 stress effects in interlaminar directions where the stress limits can be significantly lower than in-plane stress limits. To this end, the proposed Ph...

Phase 2 SBIR

Agency: Missile Defense Agency
Topic: MDA10-023
Budget: 09/24/12 - 09/23/14

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 through the plasma. Modeling these flows requires both expertise and substantial user time. The Phase II program will address these issues by developin...

Phase 1 SBIR

Agency: Air Force
Topic: AF112-004
Budget: 09/08/11 - 09/08/12

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 rapid design, simulation, and optimization of scramjet engines within an airframe-integrated context. A successful effort will produce a scramjet e...

Phase 2 SBIR

Agency: Air Force
Topic: AF093-182
Budget: 06/29/11 - 09/30/13

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-starting scramjet inlet. Under our Phase I SBIR work, we have developed and validated a self-starting inward-turning scramjet inlet concept and created ...

Phase 1 SBIR

Agency: Missile Defense Agency
Topic: MDA10-023
Budget: 06/27/11 - 01/09/12

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 through the plasma. Ablative heat shields may further increase the levels of electrons in the plasma around the hardbody and in the wake. We propose to e...

Phase 1 SBIR

Agency: Air Force
Topic: AF093-182
Budget: 03/02/10 - 01/02/11

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 design and optimization tools and will be validated with the experimental testing of a self-starting inlet in GHI s supersonic wind tunnel facility....

Phase 1 SBIR

Agency: Air Force
Topic: AF093-004
Budget: 01/20/10 - 06/30/11

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 enable us to quickly evaluate and fix problems with existing designs and quickly develop new designs with well thought out diagnostics, this would enabl...

Phase 2 SBIR

Agency: Air Force
Topic: AF073-091
Budget: 10/01/09 - 06/30/11

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 in the Mach 0-4 range. Tools will be created to permit high-fidelity conceptual designs, including viscous CFD-based optimization of the propulsiv...

Phase 1 SBIR

Agency: Air Force
Topic: AF073-091
Budget: 01/03/08 - 11/29/08

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 our Propulsion-Airframe Integration (PAI) tool, Eco. Once integrated into Eco, representative TBCC and RBCC combined-cycle air-vehicle concepts will...

Phase 1 SBIR

Agency: Air Force
Topic: AF073-058
Budget: 12/14/07 - 09/14/08

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 on engine and vehicle performance from a systems level perspective. To accomplish this, our team proposes to integrate new inlet, nozzle, and vehi...

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