Vector Launch, Llc
Dba Vector
CAGE Code: 7MLT0
NCAGE Code: 7MLT0
Status: Active
Type: Commercial Supplier
Summary
Vector Launch, Llc, Dba Vector is an Active Commercial Supplier with the Cage Code 7MLT0.
Address
15261 Connector Ln
Huntington Beach CA 92649-1117
United States
Points of Contact
No Points of Contact...
Related Information
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Frequently Asked Questions (FAQ) for CAGE 7MLT0
- What is CAGE Code 7MLT0?
- 7MLT0 is the unique identifier used by NATO Organizations to reference the physical entity known as Vector Launch, Llc Dba Vector located at 15261 Connector Ln, Huntington Beach CA 92649-1117, United States.
- Who is CAGE Code 7MLT0?
- 7MLT0 refers to Vector Launch, Llc Dba Vector located at 15261 Connector Ln, Huntington Beach CA 92649-1117, United States.
- Where is CAGE Code 7MLT0 Located?
- CAGE Code 7MLT0 is located in Huntington Beach, CA, USA.
Contracting History for CAGE 7MLT0 Most Recent 25 Records
- 80NSSC18C0150
- Eo14042 Vector Launch, Inc. Proposes To Apply Recent Advances In Micropump And Additive Manufacturing Technologies To Develop And Demonstrate A Micropump-Based Autogenous Pressurization System For Its Commercial Vector-R And Mature The Technology With Multiple Static-Fire-Tests Leading To A Demonstration Flight Test (Trl 6). The Vector-R Is A 2-Stage Pressure-Fed, Lox/Subcooled Propylene Commercial Small Launch Vehicle, Designed To Place Up To 60 Kg In Low Earth Orbit. Electrically-Driven Micropumps Drive A Small Portion Of Each Propellant Over A Novel 3D-Printed Heat Exchanger At The Engine To Pressurize The Tanks. Excess Flow Can Be Diverted To The Engine As Needed. This Approach Reduces System Mass, Complexity And Acquisition Cost As Well As Operational Costs. It Eliminates The Need For All High-Pressure Tanks And Associated Components. It Can Be Used On Any Pressure-Fed Stage, For Launch Vehicle And In-Space Application When Using High Vapor Pressure Propellants Such As Lox/Methane Or Lox/Propane. As Such, It Is An Enabler For Missions Targeted To Use In-Situ Propellants Since The Need For A Separate Pressurant Like Helium Is Either Greatly Reduced Or Eliminated. By Leveraging Vector S Ongoing Commercially-Funded Vector-R Micro-Launcher Development, It Is Possible To Reach Trl 6-Ready System During Phase Ii And Transition To The Vector-R Operations (Trl-9) Soon After.
- 21 Jan 2022
- Eo14042 Vector Launch, Inc. Proposes To Apply Recent Advances In Micropump And Additive Manufacturing Technologies To Develop And Demonstrate A Micropump-Based Autogenous Pressurization System For Its Commercial Vector-R And Mature The Technology With Multiple Static-Fire-Tests Leading To A Demonstration Flight Test (Trl 6). The Vector-R Is A 2-Stage Pressure-Fed, Lox/Subcooled Propylene Commercial Small Launch Vehicle, Designed To Place Up To 60 Kg In Low Earth Orbit. Electrically-Driven Micropumps Drive A Small Portion Of Each Propellant Over A Novel 3D-Printed Heat Exchanger At The Engine To Pressurize The Tanks. Excess Flow Can Be Diverted To The Engine As Needed. This Approach Reduces System Mass, Complexity And Acquisition Cost As Well As Operational Costs. It Eliminates The Need For All High-Pressure Tanks And Associated Components. It Can Be Used On Any Pressure-Fed Stage, For Launch Vehicle And In-Space Application When Using High Vapor Pressure Propellants Such As Lox/Methane Or Lox/Propane. As Such, It Is An Enabler For Missions Targeted To Use In-Situ Propellants Since The Need For A Separate Pressurant Like Helium Is Either Greatly Reduced Or Eliminated. By Leveraging Vector S Ongoing Commercially-Funded Vector-R Micro-Launcher Development, It Is Possible To Reach Trl 6-Ready System During Phase Ii And Transition To The Vector-R Operations (Trl-9) Soon After.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $481,044.00
- National Aeronautics And Space Administration (Nasa)