GHKN ENGINEERING, LLC

Company Information

Company Name
GHKN ENGINEERING, LLC
Address
P.O. Box 2585
16307 NE 83rd Street
Redmond, WA, -
Phone
1 425-881-3635
URL
n/a
DUNS
89115922
Number of Employees
4
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$283,792.00
3
SBIR Phase II
$2,575,185.00
3
Chart code to be here

Award List

  1. Continuous Detonation Rocket and Air Breathing Engines

    Amount: $1,123,929.00

    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 ...

    SBIR Phase II 2010 Defense Advanced Research Projects AgencyDepartment of Defense
  2. 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 ...

    SBIR Phase I 2004 ArmyDepartment of Defense
  3. 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 ...

    SBIR Phase I 2005 ArmyDepartment of Defense
  4. 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 ...

    SBIR Phase II 2006 ArmyDepartment of Defense
  5. 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 ...

    SBIR Phase II 2004 ArmyDepartment of Defense
  6. 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 ...

    SBIR Phase I 2009 Defense Advanced Research Projects AgencyDepartment of Defense

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