GHKN Engineering, LLC

Company Information
Address 11810 Holmes Point Dr NE
Kirkland, WA, 98034-3443


Information

DUNS: 089115922

# of Employees: 2


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. Feasibility Test of Rotating Detonation Rocket Engine Using Storable Hypergolic Bipropellants

    Amount: $148,069.00

    Rotating Detonation Rocket Engines (RDRE) support continuous detonation (constant volume) combustion in an annulus rather than in the deflagration combustion chambers of conventional rockets. Superson ...

    SBIRPhase I2019Department of Defense Air Force
  2. Evaluation of Rotating Detonation Rocket Engines for Booster or Upper Stage Launch Vehicles: The Next Step Towards Flight Development

    Amount: $148,142.00

    Having previously designed, built and successfully tested a Rotating Detonation Rocket Engine (RDRE), GHKN Engineering proposes to evaluate the feasibility of RDRE technology for boost or upper stage ...

    SBIRPhase I2018Department of Defense Air Force
  3. Continuous Detonation Rocket and Air Breathing Engines

    Amount: $1,475,020.00

    GHKN Engineering, LLC teamed with Aerojet Recmond, proposes to build and test a CDRE with a number of fuels and oxidizers. Included in the proposal test program is thrust measurement, which together w ...

    SBIRPhase II2010Department of Defense Defense Advanced Research Projects Agency
  4. Continuous Detonation Rocket and Air Breathing Engines

    Amount: $98,961.00

    This proposal describes an approach to evaluate the continuous detonation phenomenon using a computational fluid dynamics (CFD) method for analyzing the critical factors needed to create a model of th ...

    SBIRPhase I2009Department of Defense Defense Advanced Research Projects Agency
  5. An Integrated Thrust Control Solution

    Amount: $729,146.00

    GHKN Engineering, LLC and Aerojet Sacramento have joined together to develop a solid rocket motor (SRM) integrated thrust control system (ITCS) adaptable for a family of missile systems. These compani ...

    SBIRPhase II2006Department of Defense Army
  6. An Integrated Thrust Control Solution

    Amount: $115,383.00

    This proposal describes a feasibility study to evaluate several concepts for integrated thrust vector control of a tactical missile. The proposed designs include a moveable aeropintle capable of movin ...

    SBIRPhase I2005Department of Defense Army
  7. A Throttling Solid Propellant Rocket Motor with Adaptive Thrust Control

    Amount: $69,448.00

    An innovative nozzle concept is proposed to enable variable thrust solid rocket motors to operate with minimal loss in efficiency over a wide thrust range. The proposed approach will also allow comman ...

    SBIRPhase I2004Department of Defense Army
  8. A Throttling Solid Propellant Rocket Motor with Adaptive Thrust Control

    Amount: $722,110.00

    This proposal addresses a Phase II program to demonstrate the validity of combining two techniques for solid rocket motor control: a moveable pintle for thrust control and an aerospike plug nozzle for ...

    SBIRPhase II2004Department of Defense Army
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