MSNW, LLC

Address

WA
Redmond, WA, 98052-3557

http://www.msnwllc.com

Information

DUNS: 44381445
# of Employees: 12

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. High Thrust-to-Power Electric Propulsion through Neutral Entrainment

    Amount: $749,619.00

    ABSTRACT: State of the art Orbital Transfer Vehicle systems and GEO transfer missions require the demanding combined requirements of both high Thrust-to-Power (greater than 150 mN/kW) and high specif ...

    STTRPhase II2014Department of Defense Air Force
  2. Combustion Enhanced Electric Propulsion

    Amount: $149,999.00

    ABSTRACT: Orbital transfer missions require a demanding combination of lightweight, flexible operation and high Thrust-to-Power (greater than 120 mN/kW) electric propulsion. Adding Neutral Entrainmen ...

    SBIRPhase I2014Air Force Department of Defense
  3. ISS Launched Cubesat Demonstration of Variable-Drag Magnetoshell Aerocapture

    Amount: $124,999.00

    Aerobraking and aerocapture have been shown to be mission enabling for deep space orbiters and manned missions, and yield dramatic cost and mass savings for near earth missions. However, high dynamic ...

    SBIRPhase I2014National Aeronautics and Space Administration
  4. Adaptive Electric Propulsion for ISRU Missions

    Amount: $125,000.00

    The Electrodeless Lorentz Force Thruster (ELF-160A) has the ability to efficiently ionize and electromagnetically accelerate a variety of propellants over a broad range of specific impulses from 1,000 ...

    SBIRPhase I2014National Aeronautics and Space Administration
  5. FRC Multi-Mode Thruster Validation Demonstration

    Amount: $748,823.00

    ABSTRACT: Modern military space systems use high specific impulse (Isp) propulsion systems to provide efficient station keeping and large delta-V orbital maneuvers. A multi-mode propulsion system uti ...

    SBIRPhase II2013Department of Defense Air Force
  6. Propulsion Optimization of Thrust though Auxiliary Entrainment of Neutrals (PROTEAN)

    Amount: $100,000.00

    ABSTRACT: State of the art Orbital Transfer Vehicle systems require the demanding combined requirements of both high Thrust-to-Power (greater than 120 mN/kW) and high specific impulse (greater than 3 ...

    STTRPhase I2012Air Force Department of Defense
  7. Ultra-Light High-Thrust Electric Propulsion with Magnetic Thrust Vectoring

    Amount: $149,999.00

    ABSTRACT: MSNW"s Electrodeless Lorentz Force (ELF) thruster will address the demanding combined requirements of light weight, high efficiency, and high thrust-to-power electric propulsion in a s ...

    SBIRPhase I2012Department of Defense Air Force
  8. Low Mass Electromagnetic Plasmoid Thruster with Integrated PPU

    Amount: $599,987.00

    The Electromagnetic Plasmoid Thruster (EMPT) is a revolutionary electric propulsion thruster and power processing (PPU) system that will allow a dramatic decrease in system mass and increase in thrust ...

    SBIRPhase II2011National Aeronautics and Space Administration
  9. A Modular Electric Propulsion System with On-Demand Power Scaling

    Amount: $99,999.00

    The Electromagnetic Plasmoid Thruster (EMPT) program demonstrated a next generation propulsion system based on the purely electromagnetic generation and Lorentz acceleration of a magnetically self-con ...

    SBIRPhase I2011National Aeronautics and Space Administration
  10. A Protoflight High Specific Power Electric Propulsion System

    Amount: $1,124,999.00

    The Electromagnetic Plasmoid Thruster (EMPT) has demonstrated the ability to ionize, electromagnetically accelerate, and eject a broad range of complex and chemically-reactive molecular gases, includi ...

    SBIRPhase II2011Defense Advanced Research Projects Agency Department of Defense

Agency Micro-sites

US Flag An Official Website of the United States Government