K T Engineering Corporation

Basic Information

238 Business Park Boulevard, Building 23B Suite J
Madison, AL, 35758-7552

Company Profile

n/a

Additional Details

Field Value
DUNS: 127963515
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 7


  1. In-Space LOX/Methane Pintle Propulsion Engine (LMPPE) Evaluation and Demonstration

    Amount: $124,823.00

    KTE's proposed innovation is the LOx/Methane Pintle Propulsion Engine or (LMPPE), which can offer higher reliability, lower cost and higher performance than conventional impinging injector-based combu ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  2. Low Cost, High Efficiency, Pressurization System for Responsive Launch Operations

    Amount: $124,351.00

    KT Engineering (KTE) is pleased to submit this proposal to address the stated need for "innovative solutions that will allow spaceport launch service providers to operate in an efficient, low cos ...

    SBIR Phase I 2012 National Aeronautics and Space Administration
  3. Dual Use Catalytically Initiated Combustor (CIC) for Rocket Engine Ignition and Thruster Applications

    Amount: $99,257.00

    This proposal responds to subtopic O2.02 "Propulsion Technologies" and the stated need to develop component technologies that will lead to future propulsion systems that are reliable and hav ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  4. Altitude Compensating Nozzle Transonic Performance Flight Demonstration

    Amount: $69,920.00

    Altitude compensating nozzles continue to be of interest for use on future launch vehicle boosters and upper stages because of their higher mission average Isp and superior packaging efficiency compar ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  5. Altitude Compensating Nozzle Design Tool

    Amount: $69,809.00

    Launch vehicle subsystem preliminary design tools that are fast, accurate, and seamlessly integrated into an electronic design and optimization environment have become an essential part of the prelimi ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  6. Segmented Launch Vehicle Risk Reduction Program

    Amount: $0.00

    A Phase II program is proposed to address fundamental technical and cost risks associated with the Segmented Launch Vehicle (SLV) concept. The SLV is an innovative, largely unexplored approach that wi ...

    SBIR Phase I 2003 Missile Defense Agency Department of Defense
  7. Segmented Launch Vehicle Risk Reduction Program

    Amount: $845,000.00

    A Phase II program is proposed to address fundamental technical and cost risks associated with the Segmented Launch Vehicle (SLV) concept. The SLV is an innovative, largely unexplored approach that wi ...

    SBIR Phase II 2003 Missile Defense Agency Department of Defense

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