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Company Information:

Company Name:
GoHypersonic Inc.
Address:
714 E. Monument Ave
Suite 119
Dayton, OH 45402-1382
Phone:
(937) 531-6678
URL:
EIN:
204822248
DUNS:
780026220
Number of Employees:
16
Woman-Owned?:
No
Minority-Owned?:
No
HUBZone-Owned?:
No

Commercialization:

Has been acquired/merged with?:
N/A
Has had Spin-off?:
N/A
Has Had IPO?:
N/A
Year of IPO:
N/A
Has Patents?:
N/A
Number of Patents:
N/A
Total Sales to Date $:
$ 0.00
Total Investment to Date $
$ 0.00
POC Title:
N/A
POC Name:
N/A
POC Phone:
N/A
POC Email:
N/A
Narrative:
N/A

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $829,876.00 8
SBIR Phase II $3,149,904.00 4

Award List:

Vehicle Integrated Inward Turning Air Breathing Engines

Award Year / Program / Phase:
2006 / SBIR / Phase II
Award Amount:
$749,941.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Lance Jacobsen, President
Abstract:
The overall objective of this proposal is to develop a tool that integrates and optimizes the design of internal scramjet engine flowlines with external aerodynamic designs of hypersonic vehicles. The design of non-optimal, manual iteration engine-integrated inward turning scramjets with waverider… More

Combined Cycle Nozzle Base Drag Reduction Methods

Award Year / Program / Phase:
2007 / SBIR / Phase I
Award Amount:
$99,949.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Lance Jacobsen, President
Abstract:
In the last few years, the renewed development of inward-turning scramjets with vehicle conformal nozzle shapes for both cruise vehicle and accelerators has led to the need for new combined cycle integration strategies for both turbine and rocket engine systems. Strategies must be developed which… More

Hypersonic Propulsion-Airframe Integration

Award Year / Program / Phase:
2008 / SBIR / Phase I
Award Amount:
$99,993.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Lance Jacobsen, President
Abstract:
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… More

Combined Cycle Propulsion Integration

Award Year / Program / Phase:
2008 / SBIR / Phase I
Award Amount:
$99,986.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Lance Jacobsen, President
Abstract:
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… More

Flight-Capable Self-Starting Scramjet Inlets

Award Year / Program / Phase:
2010 / SBIR / Phase I
Award Amount:
$99,990.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Abstract:
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… More

Innovative Aerodynamic Measurement for Integrated Hypersonic Inlets

Award Year / Program / Phase:
2010 / SBIR / Phase I
Award Amount:
$99,993.00
Agency / Branch:
DOD / USAF
Principal Investigator:
Abstract:
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… More

Combined Cycle Propulsion Integration

Award Year / Program / Phase:
2010 / SBIR / Phase II
Award Amount:
$649,986.00
Agency:
DOD
Principal Investigator:
Lance S. Jacobsen, President – (937) 531-6678
Abstract:
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… More

Advanced Reentry Vehicle and Wake Models

Award Year / Program / Phase:
2011 / SBIR / Phase I
Award Amount:
$100,000.00
Agency:
DOD
Principal Investigator:
Travis Drayna, Sr. Engineer – (651) 784-3662
Abstract:
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… More

Advanced Analysis and Design Tool for Scramjet Air-frame Propulsion Integration

Award Year / Program / Phase:
2011 / SBIR / Phase I
Award Amount:
$149,988.00
Agency:
DOD
Principal Investigator:
Lance Jacobsen, President – (937) 531-6678
Abstract:
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… More

Flight-Capable Self-Starting Scramjet Inlets

Award Year / Program / Phase:
2011 / SBIR / Phase II
Award Amount:
$749,979.00
Agency:
DOD
Principal Investigator:
Lance Jacobsen, President – (937) 531-6678
Abstract:
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… More

Reentry Vehicle and Wake Analysis Tool

Award Year / Program / Phase:
2012 / SBIR / Phase II
Award Amount:
$999,998.00
Agency:
DOD
Principal Investigator:
Travis Drayna, Principal Engineer – (612) 354-7738
Abstract:
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… More

Non-Linear Damage Model for Carbon-Carbon Composite Design

Award Year / Program / Phase:
2014 / SBIR / Phase I
Award Amount:
$79,977.00
Agency / Branch:
DOD / NAVY
Principal Investigator:
Zachary Gaston, Senior Engineer – (937) 531-6678
Abstract:
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… More