GOHYPERSONIC INCORPORATED

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 ...

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 ...

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 ...

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 ...

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 ...

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 ...

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 ...

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 ...

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 inte ...

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. Th ...