Firestar Engineering, LLC

Company Information
Address 1124 Flightline St #64
Mojave, CA, 93501-1610


Information

DUNS: 119834419

# of Employees: 4


Ownership Information

Hubzone Owned: Y

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  1. SBIR Phase I: Thermal Engine with Metastable Power Extraction Step (TEMPES)

    Amount: $149,980.00

    This Small Business Innovation Research (SBIR) Phase I project will develop critical measurements necessary for eventually producing a high efficiency Thermal Engine with Metastable Power Extraction S ...

    SBIRPhase I2014National Science Foundation
  2. Low Energy Electronic Ignition System for NOFBX Thrusters

    Amount: $696,448.00

    NOFBX propulsion technology is being developed actively for a number of applications including a flight experiment on the International Space Station NOFBX propellant has unique electrical properties ...

    SBIRPhase II2013National Aeronautics and Space Administration
  3. Low Energy Electronic Ignition System for NOFBX Thrusters

    Amount: $124,958.00

    We propose to develop a miniature, low RF noise ignition module for NOFBX propulsion systems. This ignition module is designed utilizing unique properties of the NOFBX propellant to enable a potential ...

    SBIRPhase I2012National Aeronautics and Space Administration
  4. NOFBX Single-Stage-to-Orbit Mars Ascent Vehicle Engine

    Amount: $589,173.00

    We propose the continuation of our research and development of a Nitrous Oxide Fuel Blend (NOFBXTM) Single-Stage-to-Orbit (SSTO) monopropellant propulsion system for future use on a Mars Ascent Vehicl ...

    SBIRPhase II2011National Aeronautics and Space Administration
  5. Low Cost Carbon-Carbon Rocket Nozzle Development

    Amount: $99,672.00

    This development will provide an inexpensive vacuum nozzle manufacturing option for NOFBX<SUP>TM</SUP> monopropellant systems that are currently being developed under NASA SBIR funding. NO ...

    SBIRPhase I2011National Aeronautics and Space Administration
  6. NOFB-Aerospike

    Amount: $99,790.00

    We propose the research, development and testing of a clustered aerospike engine to eventually be utilized with our high performance NOFB (nitrous oxide fuel blend) monopropellant and combustion chamb ...

    SBIRPhase I2010National Aeronautics and Space Administration
  7. Nitrous Oxide Fuel Blend-Continuous Operation Lunar Thruster (NOFB-COLT)

    Amount: $599,976.00

    Firestar Engineering has developed a set of Nitrous Oxide Fuel Blend monopropellants that are: 1) Non-toxic, 2) Specific Impulse> 310 s, 3) Freezing point < -77 C, 4) Self Pressurizing, and 5) Highl ...

    SBIRPhase II2009National Aeronautics and Space Administration
  8. Very High Altitude Aircraft Propulsion Engines

    Amount: $1,124,870.00

    Firestar Engineering, LLC has been exploring the use of NOFB monopropellants for use in very high altitude unmanned aerial vehicle applications. Monopropellants remove the requirement for ingesting ai ...

    SBIRPhase II2009Defense Advanced Research Projects Agency Department of Defense
  9. Nitrous Oxide Fuel Blend-Continuous Operation Lunar Thruster (NOFB-COLT)

    Amount: $96,152.00

    We propose conducting further development for a Nitrous Oxide Fuel Blend (NOFB) propulsion system. Phase I activities will concentrate on a revising a previous 5 lbf thruster to facilitate continuous ...

    SBIRPhase I2008National Aeronautics and Space Administration
  10. Very High Altitude Aircraft Propulsion Engines

    Amount: $98,303.00

    Firestar Engineering proposes a compact 4 cylinder, boxer style, piston engine that uses a NOFB3x series monopropellant to facilitate extreme altitude flight for long durations. This 4 cylinder engin ...

    SBIRPhase I2007Defense Advanced Research Projects Agency Department of Defense

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