T.G.V. Rockets Inc.
Dba Tgv Rockets Inc
CAGE Code: 3CF24
NCAGE Code: 3CF24
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 799713594
Summary
T.G.V. Rockets Inc., Dba Tgv Rockets Inc is an Active Commercial Supplier with the Cage Code 3CF24 and is tracked by Dun & Bradstreet under DUNS Number 799713594..
Address
2519 Benning Rd Ne
Washington DC 20002-4805
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 3CF24
- What is CAGE Code 3CF24?
- 3CF24 is the unique identifier used by NATO Organizations to reference the physical entity known as T.G.V. Rockets Inc. Dba Tgv Rockets Inc located at 2519 Benning Rd Ne, Washington DC 20002-4805, United States.
- Who is CAGE Code 3CF24?
- 3CF24 refers to T.G.V. Rockets Inc. Dba Tgv Rockets Inc located at 2519 Benning Rd Ne, Washington DC 20002-4805, United States.
- Where is CAGE Code 3CF24 Located?
- CAGE Code 3CF24 is located in Washington, DC, USA.
Contracting History for CAGE 3CF24 Most Recent 25 Records
- FA930023C6027
- 873Authority Deep Throttling, Liquid, Bi Propellant Rocket Engine
- 26 Sep 2023
- 873Authority Deep Throttling, Liquid, Bi Propellant Rocket Engine
- Fa9300 Aftc Pzr
- Department Of Defense (Dod)
- $4,498,342.00
- Department Of Defense (Dod)
- N6833523C0378
- Kick-Off Briefing Materials & Fwa Cert.
- 12 Jun 2023
- Kick-Off Briefing Materials & Fwa Cert.
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $139,804.00
- Department Of Defense (Dod)
- 80NSSC22PB220
- E014042 Sbir Phase I Solid State Welding For Space
- 21 Jul 2022
- E014042 Sbir Phase I Solid State Welding For Space
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $149,821.00
- National Aeronautics And Space Administration (Nasa)
- FA930022C6030
- Research And Development Of The Altitude Compensating, Lobed Nozzle
- 11 Jul 2023
- Research And Development Of The Altitude Compensating, Lobed Nozzle
- Fa9300 Aftc Pzr
- Department Of Defense (Dod)
- $2,098,169.84
- Department Of Defense (Dod)
- N6833521C0690
- Research And Development
- 2 Aug 2021
- Research And Development
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $139,916.67
- Department Of Defense (Dod)
- FA864921P0528
- Smart Valves For Smart Rocket Engines
- 5 Feb 2021
- Smart Valves For Smart Rocket Engines
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $49,899.00
- Department Of Defense (Dod)
- FA864921P1414
- Single Stage Reusable Launch Vehicles For Resilient Space Launch
- 12 Apr 2021
- Single Stage Reusable Launch Vehicles For Resilient Space Launch
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $49,792.00
- Department Of Defense (Dod)
- FA864921C0013
- Low Cost Expendable Launch Technology
- 12 Oct 2021
- Low Cost Expendable Launch Technology
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $749,837.00
- Department Of Defense (Dod)
- FA864921C0013
- Testing And Evaluation Of Rocket Engine Using Propoly Fuel At Cyrogenic And Non Cyrogenic Temperatures
- 15 Jan 2021
- Testing And Evaluation Of Rocket Engine Using Propoly Fuel At Cyrogenic And Non Cyrogenic Temperatures
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $749,837.00
- Department Of Defense (Dod)
- 80NSSC21C0343
- Development Of Advanced Joining Technologies, Large-Scale Additive Manufacturing Processes, And Metal Recycling Technologies For On-Orbit Manufacturing
- 29 Nov 2021
- Development Of Advanced Joining Technologies, Large-Scale Additive Manufacturing Processes, And Metal Recycling Technologies For On-Orbit Manufacturing
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,881.00
- National Aeronautics And Space Administration (Nasa)
- NNX17CM59P
- Igf::Ot::Igf Nasa Is Extremely Interested In Developing Small Space Launch Capability. Small Launchers Are More Sensitive To Dry Mass Growth, More So Then Larger Vehicles. Three Stage Launchers Tend To Be Much More Insensitive To Dry Mass Growth. The Challenge Then Becomes How To Meet Strict Cost Targets When Additional Parts Count Increases. Use Of Propane Derived Fuel Helps Reduce Cost By Allowing Common Bulkhead Tanks W/O Insulation. Tgv Proposes A Darpa Funded Electrocycle Boost Stage, And A Nasa Funded Pressure Fed Micro Stage. Upgrade Nasa Sttr Funded Nano-Stage With 3,000 Class Pressure Fed Second Stage Propoly 50 Engine. Goal: Provide Flexible Architecture To Ensure Success Of Tgv's 15,000 Lb Class First Stage And 500 Lbs Class Upper Stage. Design And Build Engine In Phase I. No Avionics, Strictly Middle Stage. Could Be Used For Suborbital Testing Of Small Upper Stages. Phase Ii: Test Engine, Build Stage, Fly.
- 8 Jun 2018
- Igf::Ot::Igf Nasa Is Extremely Interested In Developing Small Space Launch Capability. Small Launchers Are More Sensitive To Dry Mass Growth, More So Then Larger Vehicles. Three Stage Launchers Tend To Be Much More Insensitive To Dry Mass Growth. The Challenge Then Becomes How To Meet Strict Cost Targets When Additional Parts Count Increases. Use Of Propane Derived Fuel Helps Reduce Cost By Allowing Common Bulkhead Tanks W/O Insulation. Tgv Proposes A Darpa Funded Electrocycle Boost Stage, And A Nasa Funded Pressure Fed Micro Stage. Upgrade Nasa Sttr Funded Nano-Stage With 3,000 Class Pressure Fed Second Stage Propoly 50 Engine. Goal: Provide Flexible Architecture To Ensure Success Of Tgv's 15,000 Lb Class First Stage And 500 Lbs Class Upper Stage. Design And Build Engine In Phase I. No Avionics, Strictly Middle Stage. Could Be Used For Suborbital Testing Of Small Upper Stages. Phase Ii: Test Engine, Build Stage, Fly.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,123.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0343
- Development Of Advanced Joining Technologies, Large-Scale Additive Manufacturing Processes, And Metal Recycling Technologies For On-Orbit Manufacturing
- 20 Aug 2021
- Development Of Advanced Joining Technologies, Large-Scale Additive Manufacturing Processes, And Metal Recycling Technologies For On-Orbit Manufacturing
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,881.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2170
- Nasa Has Identified Nuclear Thermal Propulsion (Ntp) As An Advanced Propulsion Concept For Human Missions To Mars. It Is Seeking Technologies Related To Ntp For Development Of The Reactors And Technologies Needed For Ground Testing. In The Area Of Ground Testing, Nasa Is Interested In Approaches To Efficiently Generate High Temperature, High Flow Rate Hydrogen. Tgv Rockets, Inc., Proposes Development Of A Modular Pump Based On Tgv S Electrocycle Motor Technology To Augment A Ntp Propellant Management System. The Pump Is Based On Tgv S Electrocycle Motor Technology Utilizes Cryogenic Cooling To Boost Power Density To Levels On The Order Of 11 Hp/Lb, Making It Competitive With Conventional Gas Turbine Technologies. The Electopump Approach Offers The Advantage Of Predictable Flow Control, Real Time Engine Health Management, And Tailored Mixture Ratio Control For Improved Performance. Specific Applications Include Boosting Main Turbopump Performance, Smoothing Start-Up Transients, Improving Shutdown Cooling, And Distributed Flow Management . The Specific Research Will Size A Motor And Pump To Address Ntp Start-Up Transients, Evaluate Design Trades, Determine Power And Thermal Requirements, And Further Investigate Opportunities To Apply The Electropump For Performance Improvement And Reduction Of Safety Risks.
- 23 Jul 2018
- Nasa Has Identified Nuclear Thermal Propulsion (Ntp) As An Advanced Propulsion Concept For Human Missions To Mars. It Is Seeking Technologies Related To Ntp For Development Of The Reactors And Technologies Needed For Ground Testing. In The Area Of Ground Testing, Nasa Is Interested In Approaches To Efficiently Generate High Temperature, High Flow Rate Hydrogen. Tgv Rockets, Inc., Proposes Development Of A Modular Pump Based On Tgv S Electrocycle Motor Technology To Augment A Ntp Propellant Management System. The Pump Is Based On Tgv S Electrocycle Motor Technology Utilizes Cryogenic Cooling To Boost Power Density To Levels On The Order Of 11 Hp/Lb, Making It Competitive With Conventional Gas Turbine Technologies. The Electopump Approach Offers The Advantage Of Predictable Flow Control, Real Time Engine Health Management, And Tailored Mixture Ratio Control For Improved Performance. Specific Applications Include Boosting Main Turbopump Performance, Smoothing Start-Up Transients, Improving Shutdown Cooling, And Distributed Flow Management . The Specific Research Will Size A Motor And Pump To Address Ntp Start-Up Transients, Evaluate Design Trades, Determine Power And Thermal Requirements, And Further Investigate Opportunities To Apply The Electropump For Performance Improvement And Reduction Of Safety Risks.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $122,528.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2170
- Nasa Has Identified Nuclear Thermal Propulsion (Ntp) As An Advanced Propulsion Concept For Human Missions To Mars. It Is Seeking Technologies Related To Ntp For Development Of The Reactors And Technologies Needed For Ground Testing. In The Area Of Ground Testing, Nasa Is Interested In Approaches To Efficiently Generate High Temperature, High Flow Rate Hydrogen. Tgv Rockets, Inc., Proposes Development Of A Modular Pump Based On Tgv S Electrocycle Motor Technology To Augment A Ntp Propellant Management System. The Pump Is Based On Tgv S Electrocycle Motor Technology Utilizes Cryogenic Cooling To Boost Power Density To Levels On The Order Of 11 Hp/Lb, Making It Competitive With Conventional Gas Turbine Technologies. The Electopump Approach Offers The Advantage Of Predictable Flow Control, Real Time Engine Health Management, And Tailored Mixture Ratio Control For Improved Performance. Specific Applications Include Boosting Main Turbopump Performance, Smoothing Start-Up Transients, Improving Shutdown Cooling, And Distributed Flow Management . The Specific Research Will Size A Motor And Pump To Address Ntp Start-Up Transients, Evaluate Design Trades, Determine Power And Thermal Requirements, And Further Investigate Opportunities To Apply The Electropump For Performance Improvement And Reduction Of Safety Risks.
- 23 Jul 2018
- Nasa Has Identified Nuclear Thermal Propulsion (Ntp) As An Advanced Propulsion Concept For Human Missions To Mars. It Is Seeking Technologies Related To Ntp For Development Of The Reactors And Technologies Needed For Ground Testing. In The Area Of Ground Testing, Nasa Is Interested In Approaches To Efficiently Generate High Temperature, High Flow Rate Hydrogen. Tgv Rockets, Inc., Proposes Development Of A Modular Pump Based On Tgv S Electrocycle Motor Technology To Augment A Ntp Propellant Management System. The Pump Is Based On Tgv S Electrocycle Motor Technology Utilizes Cryogenic Cooling To Boost Power Density To Levels On The Order Of 11 Hp/Lb, Making It Competitive With Conventional Gas Turbine Technologies. The Electopump Approach Offers The Advantage Of Predictable Flow Control, Real Time Engine Health Management, And Tailored Mixture Ratio Control For Improved Performance. Specific Applications Include Boosting Main Turbopump Performance, Smoothing Start-Up Transients, Improving Shutdown Cooling, And Distributed Flow Management . The Specific Research Will Size A Motor And Pump To Address Ntp Start-Up Transients, Evaluate Design Trades, Determine Power And Thermal Requirements, And Further Investigate Opportunities To Apply The Electropump For Performance Improvement And Reduction Of Safety Risks.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $122,528.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2170
- Nasa Has Identified Nuclear Thermal Propulsion (Ntp) As An Advanced Propulsion Concept For Human Missions To Mars. It Is Seeking Technologies Related To Ntp For Development Of The Reactors And Technologies Needed For Ground Testing. In The Area Of Ground Testing, Nasa Is Interested In Approaches To Efficiently Generate High Temperature, High Flow Rate Hydrogen. Tgv Rockets, Inc., Proposes Development Of A Modular Pump Based On Tgv S Electrocycle Motor Technology To Augment A Ntp Propellant Management System. The Pump Is Based On Tgv S Electrocycle Motor Technology Utilizes Cryogenic Cooling To Boost Power Density To Levels On The Order Of 11 Hp/Lb, Making It Competitive With Conventional Gas Turbine Technologies. The Electopump Approach Offers The Advantage Of Predictable Flow Control, Real Time Engine Health Management, And Tailored Mixture Ratio Control For Improved Performance. Specific Applications Include Boosting Main Turbopump Performance, Smoothing Start-Up Transients, Improving Shutdown Cooling, And Distributed Flow Management . The Specific Research Will Size A Motor And Pump To Address Ntp Start-Up Transients, Evaluate Design Trades, Determine Power And Thermal Requirements, And Further Investigate Opportunities To Apply The Electropump For Performance Improvement And Reduction Of Safety Risks.
- 12 Feb 2019
- Nasa Has Identified Nuclear Thermal Propulsion (Ntp) As An Advanced Propulsion Concept For Human Missions To Mars. It Is Seeking Technologies Related To Ntp For Development Of The Reactors And Technologies Needed For Ground Testing. In The Area Of Ground Testing, Nasa Is Interested In Approaches To Efficiently Generate High Temperature, High Flow Rate Hydrogen. Tgv Rockets, Inc., Proposes Development Of A Modular Pump Based On Tgv S Electrocycle Motor Technology To Augment A Ntp Propellant Management System. The Pump Is Based On Tgv S Electrocycle Motor Technology Utilizes Cryogenic Cooling To Boost Power Density To Levels On The Order Of 11 Hp/Lb, Making It Competitive With Conventional Gas Turbine Technologies. The Electopump Approach Offers The Advantage Of Predictable Flow Control, Real Time Engine Health Management, And Tailored Mixture Ratio Control For Improved Performance. Specific Applications Include Boosting Main Turbopump Performance, Smoothing Start-Up Transients, Improving Shutdown Cooling, And Distributed Flow Management . The Specific Research Will Size A Motor And Pump To Address Ntp Start-Up Transients, Evaluate Design Trades, Determine Power And Thermal Requirements, And Further Investigate Opportunities To Apply The Electropump For Performance Improvement And Reduction Of Safety Risks.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $122,528.00
- National Aeronautics And Space Administration (Nasa)
- HQ014719C7074
- Sbir/Sttr Phase I Research&Development: Safe Upper Stage Engine (Suse) W/ Nitrous Oxide And Thermal Enhanced Additive Fuel.
- 26 Mar 2019
- Sbir/Sttr Phase I Research&Development: Safe Upper Stage Engine (Suse) W/ Nitrous Oxide And Thermal Enhanced Additive Fuel.
- Missile Defense Agency (Mda)
- Department Of Defense (Dod)
- $99,904.62
- Department Of Defense (Dod)
- 80NSSC18P2151
- Design And Manufacture Of A Liquid Fuel Injector Optimized For Ultrasonic Additive Manufacturing. Uam Delivers Aerospace Parts Today At 97% Of Bulk Material Property And Foil Laydown Rates At Speeds Significantly Better Then Powder Or Filament Process. Uam Has Traditionally Been Applied To 2-D Planar Surfaces. We Will Extend Uam Into Complex Geometries And Constructs Suitable For Rocket Engine Injectors.
- 4 Oct 2019
- Design And Manufacture Of A Liquid Fuel Injector Optimized For Ultrasonic Additive Manufacturing. Uam Delivers Aerospace Parts Today At 97% Of Bulk Material Property And Foil Laydown Rates At Speeds Significantly Better Then Powder Or Filament Process. Uam Has Traditionally Been Applied To 2-D Planar Surfaces. We Will Extend Uam Into Complex Geometries And Constructs Suitable For Rocket Engine Injectors.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,093.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0343
- Development Of Advanced Joining Technologies, Large-Scale Additive Manufacturing Processes, And Metal Recycling Technologies For On-Orbit Manufacturing
- 15 May 2021
- Development Of Advanced Joining Technologies, Large-Scale Additive Manufacturing Processes, And Metal Recycling Technologies For On-Orbit Manufacturing
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,881.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2151
- Design And Manufacture Of A Liquid Fuel Injector Optimized For Ultrasonic Additive Manufacturing. Uam Delivers Aerospace Parts Today At 97% Of Bulk Material Property And Foil Laydown Rates At Speeds Significantly Better Then Powder Or Filament Process. Uam Has Traditionally Been Applied To 2-D Planar Surfaces. We Will Extend Uam Into Complex Geometries And Constructs Suitable For Rocket Engine Injectors.
- 25 Jul 2018
- Design And Manufacture Of A Liquid Fuel Injector Optimized For Ultrasonic Additive Manufacturing. Uam Delivers Aerospace Parts Today At 97% Of Bulk Material Property And Foil Laydown Rates At Speeds Significantly Better Then Powder Or Filament Process. Uam Has Traditionally Been Applied To 2-D Planar Surfaces. We Will Extend Uam Into Complex Geometries And Constructs Suitable For Rocket Engine Injectors.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,093.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2151
- Design And Manufacture Of A Liquid Fuel Injector Optimized For Ultrasonic Additive Manufacturing. Uam Delivers Aerospace Parts Today At 97% Of Bulk Material Property And Foil Laydown Rates At Speeds Significantly Better Then Powder Or Filament Process. Uam Has Traditionally Been Applied To 2-D Planar Surfaces. We Will Extend Uam Into Complex Geometries And Constructs Suitable For Rocket Engine Injectors.
- 25 Jul 2018
- Design And Manufacture Of A Liquid Fuel Injector Optimized For Ultrasonic Additive Manufacturing. Uam Delivers Aerospace Parts Today At 97% Of Bulk Material Property And Foil Laydown Rates At Speeds Significantly Better Then Powder Or Filament Process. Uam Has Traditionally Been Applied To 2-D Planar Surfaces. We Will Extend Uam Into Complex Geometries And Constructs Suitable For Rocket Engine Injectors.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,093.00
- National Aeronautics And Space Administration (Nasa)