MACH I Inc.

Basic Information

340 East Church Road
King of Prussia, PA, -

http://www.machichemicals.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 153985650
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 8


  1. New Energetic Solid Propellant Ingredients

    Amount: $499,763.00

    MACH I Inc. propose to extend the technology developed under a previous Phase II STTR. This new technology will transition the demonstrated performance advantages to a commercial system, the Joint Mul ...

    STTR Phase II 2011 Navy Department of Defense
  2. A Process to Make Propulsion Grade Functional Polybutadiene

    Amount: $730,000.00

    In 1997, MACH I, Inc. was awarded a Phase I SBIR contract F42650-97-C-0400"A Process to Manufacture Carboxyl Terminated Polybutadiene (CTPB)."MACH I successfully completed this research and ...

    SBIR Phase II 2011 Department of Defense Army
  3. New Energetic Solid Propellant Ingredients

    Amount: $749,991.00

    Boron has significant potential as a high energy density fuel in munitions and propellants. Its superior energy density makes it attractive as a fuel component in conventional solid propellants, as w ...

    STTR Phase II 2006 Department of Defense Air Force
  4. Fuel Processor Hardware Components For Deployable Fuel Cell Power Generation

    Amount: $99,995.00

    The objectives for this SBIR Phase I study are to establish feasibility for deployable logistic-fuel processor to produce a clean hydrogen gas (sulfur free) from JP-8 fuel. The processor is a portabl ...

    SBIR Phase I 2005 Air Force Department of Defense
  5. New Energetic Solid Propellant Ingredients

    Amount: $99,106.00

    Boron has significant potential as a high energy density ingredient in ramjet propellants and fuels. This is due to boron's high heat of combustion and low atomic weight. For a ramjet ducted rocket ...

    STTR Phase I 2005 Department of Defense Air Force
  6. High Density Impulse Propellants

    Amount: $656,585.00

    Solid propellants with significantly higher density impulse versus conventional aluminum propellants can be prepared utilizing zirconium metal fuel. This has been independently demonstrated by severa ...

    SBIR Phase II 2003 Missile Defense Agency Department of Defense
  7. Advanced Divert and Attitude Control

    Amount: $69,980.00

    Gel bi-propulsion systems can be used as bi-propellant systems utilizing advanced energy management for increasing the performance of missiles. Improved Divert and Attitude Control (DACS) technology ...

    SBIR Phase I 2003 Missile Defense Agency Department of Defense
  8. Low Temperature Nanoscale Catalyst for Reduced Toxicity Monopropellant

    Amount: $717,308.00

    "The Aviation and Missile Command developed CINCH (Competitive Impulse Non-Carcinogenic Hypergol) fuel as a reduced toxicity alternative to carcinogenic hydrazines in propellant applications. Unfor ...

    SBIR Phase II 2002 Army Department of Defense
  9. Robust, Highly Producible Gel Propellants Formulated for Improved Performance, Reduced Toxicity, and Extended Storability

    Amount: $69,981.00

    "Gel bi-propulsion systems can be used as simple boosters and variable thrusters forNASA launch vehicles, spacecraft and satellites as well as bi-propellant systemsutilizing advanced energy management ...

    SBIR Phase I 2002 Missile Defense Agency Department of Defense
  10. Low Temperature Nanoscale Catalyst for Reduced Toxicity Monopropellant

    Amount: $118,878.00

    Toxic hydrazines with iridium catalysts are currently used in monpropellant andgas generator applications. NASA estimated handling carcenogenic hydrazines adds$500,000 cost to each space shuttle miss ...

    SBIR Phase I 2001 Army Department of Defense

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