Msnw Llc
Dba Msnw
CAGE Code: 1SDB3
NCAGE Code: 1SDB3
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 044381445
Summary
Msnw Llc, Dba Msnw is an Active Commercial Supplier with the Cage Code 1SDB3 and is tracked by Dun & Bradstreet under DUNS Number 044381445..
Address
16436 Se 39Th Pl
Bellevue WA 98008-5858
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 1SDB3
- What is CAGE Code 1SDB3?
- 1SDB3 is the unique identifier used by NATO Organizations to reference the physical entity known as Msnw Llc Dba Msnw located at 16436 Se 39Th Pl, Bellevue WA 98008-5858, United States.
- Who is CAGE Code 1SDB3?
- 1SDB3 refers to Msnw Llc Dba Msnw located at 16436 Se 39Th Pl, Bellevue WA 98008-5858, United States.
- Where is CAGE Code 1SDB3 Located?
- CAGE Code 1SDB3 is located in Bellevue, WA, USA.
Contracting History for CAGE 1SDB3 Most Recent 25 Records
- IND11PC20180
- A Protoflight High Specific Power Electric Propulsion System
- 19 Jul 2022
- A Protoflight High Specific Power Electric Propulsion System
- Ibc Acq Svcs Directorate (00004)
- Department Of The Interior (Doi)
- $1,250,246.22
- Department Of The Interior (Doi)
- NNH15CN80C
- Next Space Technologies For Exploration Partnerships Nextstep) Baa, Hi-Power Electric Propulsion Test Demonstration. The Msnw Elf-250 Will Provide Dramatic Advancements In Mass, Service Life, Throttleable Power, Efficiency Across A Broad Power Range, And Propellant Flexibility Over Existing High-Power Electric Propulsion Devices. Proposed Is A Development Plan To Develop The Thruster For High-Power, Exploration Class Missions. Nominally, The Thruster Is A Nominal 100 Joules Per Pulse, That Is Designed For Average Powers Of 100-500 Kw Steady State, With Operation At 1000-5000 Seconds Specific Impulse (Isp) On Xenon And 2000-8000 S Isp On Argon. It Is Expected From Previous Steady Operating And Lower Power Thruster Designs That A Thruster And Ppu Combination Will Be Less Than 3 Kg/Kw, If Not Dramatically Less. Unlike Any Steady State Electric Propulsion System To Date, The Elf-250 Can Be Tested At Full Power, At Limited Pulse Duty Cycle, In Existing Testing Facilities. The Elf Thruster Family Have A Design History With All Operational Physics Demonstrated Up To The 1 Mw Scale, And Many Technical Challenges Addressed Up The 30 Kw Level. The Elf Is Well Suited For Nasa Exploration-Class Missions And Would Be Both Transformational As Well As Complementary To Existing High Power Electric Propulsion Development Efforts. The 250 Mm Diameter Electrodeless Lorentz Force (Elf-250) Thruster Creates A High-Density, Magnetized Plasmoid Known As A Field Reversed Configuration (Frc) Employing A Rotating Magnetic Field (Rmf). The Rmf Driven Azimuthal Currents, Coupled With The Enhanced Axial Magnetic Field Gradient Produced By The Frc Inside The Flux Preserving Conical Thruster, Produce A Large Axial Jxbr Force That Accelerates The Plasmoid To High Velocity. Higher Internal Plasma Temperatures And Densities Significantly Reduce Ionization Losses Over Traditional Ep, While Plasma Expansion Minimizes Thermal And Frozen Flow Losses Maximizing Overall Efficiency While At The Same Time Decrease Thruster Footprint And Weight. In This Nextstep Baa A Partnership Between Msnw Llc And The University Of Washington Will Develop And Test A Propulsion System Capable Of Operation From 100 To 300 Kw Power And 2000 To 5000 S Specific Impulse On Both Traditional And In-Situ Propellants.
- 30 Aug 2021
- Next Space Technologies For Exploration Partnerships Nextstep) Baa, Hi-Power Electric Propulsion Test Demonstration. The Msnw Elf-250 Will Provide Dramatic Advancements In Mass, Service Life, Throttleable Power, Efficiency Across A Broad Power Range, And Propellant Flexibility Over Existing High-Power Electric Propulsion Devices. Proposed Is A Development Plan To Develop The Thruster For High-Power, Exploration Class Missions. Nominally, The Thruster Is A Nominal 100 Joules Per Pulse, That Is Designed For Average Powers Of 100-500 Kw Steady State, With Operation At 1000-5000 Seconds Specific Impulse (Isp) On Xenon And 2000-8000 S Isp On Argon. It Is Expected From Previous Steady Operating And Lower Power Thruster Designs That A Thruster And Ppu Combination Will Be Less Than 3 Kg/Kw, If Not Dramatically Less. Unlike Any Steady State Electric Propulsion System To Date, The Elf-250 Can Be Tested At Full Power, At Limited Pulse Duty Cycle, In Existing Testing Facilities. The Elf Thruster Family Have A Design History With All Operational Physics Demonstrated Up To The 1 Mw Scale, And Many Technical Challenges Addressed Up The 30 Kw Level. The Elf Is Well Suited For Nasa Exploration-Class Missions And Would Be Both Transformational As Well As Complementary To Existing High Power Electric Propulsion Development Efforts. The 250 Mm Diameter Electrodeless Lorentz Force (Elf-250) Thruster Creates A High-Density, Magnetized Plasmoid Known As A Field Reversed Configuration (Frc) Employing A Rotating Magnetic Field (Rmf). The Rmf Driven Azimuthal Currents, Coupled With The Enhanced Axial Magnetic Field Gradient Produced By The Frc Inside The Flux Preserving Conical Thruster, Produce A Large Axial Jxbr Force That Accelerates The Plasmoid To High Velocity. Higher Internal Plasma Temperatures And Densities Significantly Reduce Ionization Losses Over Traditional Ep, While Plasma Expansion Minimizes Thermal And Frozen Flow Losses Maximizing Overall Efficiency While At The Same Time Decrease Thruster Footprint And Weight. In This Nextstep Baa A Partnership Between Msnw Llc And The University Of Washington Will Develop And Test A Propulsion System Capable Of Operation From 100 To 300 Kw Power And 2000 To 5000 S Specific Impulse On Both Traditional And In-Situ Propellants.
- Nasa Headquarters
- National Aeronautics And Space Administration (Nasa)
- $1,250,000.00
- National Aeronautics And Space Administration (Nasa)