Parabilis Space Technologies, Inc.
Dba Parabilis Space Technologies Inc
CAGE Code: 7BCN7
NCAGE Code: 7BCN7
Status: Active
Type: Manufacturer
Summary
Parabilis Space Technologies, Inc., Dba Parabilis Space Technologies Inc is an Active Manufacturer with the Cage Code 7BCN7.
Address
1195 Linda Vista Dr
Ste F
San Marcos CA 92078-3824
United States
Points of Contact
No Points of Contact...
Related Information
No Related Information...
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Frequently Asked Questions (FAQ) for CAGE 7BCN7
- What is CAGE Code 7BCN7?
- 7BCN7 is the unique identifier used by NATO Organizations to reference the physical entity known as Parabilis Space Technologies, Inc. Dba Parabilis Space Technologies Inc located at 1195 Linda Vista Dr, Ste F, San Marcos CA 92078-3824, United States.
- Who is CAGE Code 7BCN7?
- 7BCN7 refers to Parabilis Space Technologies, Inc. Dba Parabilis Space Technologies Inc located at 1195 Linda Vista Dr, Ste F, San Marcos CA 92078-3824, United States.
- Where is CAGE Code 7BCN7 Located?
- CAGE Code 7BCN7 is located in San Marcos, CA, USA.
Contracting History for CAGE 7BCN7 Most Recent 25 Records
- FA864922P0804
- Advanced, Modular, In-Space, Green Propulsion
- 7 Mar 2022
- Advanced, Modular, In-Space, Green Propulsion
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $749,641.00
- Department Of Defense (Dod)
- FA864922P0458
- Innovative Infrared Beacon Payload For Calibration Of Air Force Ground Sensors
- 1 Nov 2021
- Innovative Infrared Beacon Payload For Calibration Of Air Force Ground Sensors
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $49,713.00
- Department Of Defense (Dod)
- FA945321C0004
- Sbir Iii-Advanced, Economical, In-Space Hybrid Propulsion
- 10 Jun 2021
- Sbir Iii-Advanced, Economical, In-Space Hybrid Propulsion
- Fa9453 Det 8 Afrl Pkv8
- Department Of Defense (Dod)
- $1,141,505.00
- Department Of Defense (Dod)
- FA945321C0004
- Nce- Sibr Iii Advanced Economical In-Space Hybrid
- 9 Dec 2021
- Nce- Sibr Iii Advanced Economical In-Space Hybrid
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $1,141,505.00
- Department Of Defense (Dod)
- FA945321C0004
- Loa Correction Sibr Iii- Advanced Economical In-Space Hybrid
- 2 Aug 2021
- Loa Correction Sibr Iii- Advanced Economical In-Space Hybrid
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $1,141,505.00
- Department Of Defense (Dod)
- FA864921P1043
- Low-Cost, Safe, Bi-Propellant Propulsion For Smallsats
- 13 Apr 2021
- Low-Cost, Safe, Bi-Propellant Propulsion For Smallsats
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $49,918.00
- Department Of Defense (Dod)
- FA864920C0182
- Covid-19 Dib, Small Business Innovative Research Award Phase Ii, Hybrid Rocket Propulsion For Hypersonic Missile Defense Research
- 3 Jun 2020
- Covid-19 Dib, Small Business Innovative Research Award Phase Ii, Hybrid Rocket Propulsion For Hypersonic Missile Defense Research
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $1,453,770.00
- Department Of Defense (Dod)
- FA864920C0182
- Covid-19 Dib, Small Business Innovative Research Award Phase Ii, Hybrid Rocket Propulsion For Hypersonic Missile Defense Research
- 18 May 2021
- Covid-19 Dib, Small Business Innovative Research Award Phase Ii, Hybrid Rocket Propulsion For Hypersonic Missile Defense Research
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $1,453,770.00
- Department Of Defense (Dod)
- FA864920C0182
- Covid-19 Dib, Small Business Innovative Research Award Phase Ii, Hybrid Rocket Propulsion For Hypersonic Missile Defense Research
- 17 Nov 2021
- Covid-19 Dib, Small Business Innovative Research Award Phase Ii, Hybrid Rocket Propulsion For Hypersonic Missile Defense Research
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $1,453,770.00
- Department Of Defense (Dod)
- 80NSSC19C0064
- Eo14042 Parabilis Space Technologies, Inc. In Collaboration With Utah State University Proposes Further Development Of A Low Cost
- 13 Oct 2021
- Eo14042 Parabilis Space Technologies, Inc. In Collaboration With Utah State University Proposes Further Development Of A Low Cost
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,670.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0064
- Parabilis Space Technologies, Inc. In Collaboration With Utah State University Proposes Further Development Of A Low Cost, High Performance Launch Vehicle
- 4 Aug 2021
- Parabilis Space Technologies, Inc. In Collaboration With Utah State University Proposes Further Development Of A Low Cost, High Performance Launch Vehicle
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,670.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0064
- Eo14042 High Performance Hybrid Upper Stage For Nanolaunch Vehicles
- 7 Feb 2022
- Eo14042 High Performance Hybrid Upper Stage For Nanolaunch Vehicles
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,670.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0117
- Eo14042 Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing. This Innovative Capability Dramatically Adds To And Extends The Advantages Of Using A Cavitating Venturi To Isolate Combustion Chambers Or Other Downstream Process Fluctuations From Upstream Feed Pressure Conditions. This Design Will Greatly Simplify Propulsion Testing And Reduce Costs For Cases Where Desired Liquid Flow Conditions Are Either Not Precisely Understood Or Cover A Range Of High-Precision Flow Rates. The Proposed Geometry Is Capable Of Scaling To Both Ultra-High Pressure And High Flow Rate Applications. The Primary Innovation Consists Of A Unique Floating Pintle Design And Associated Structural Support With Built-In Pressure Taps. These Printed-In Pressure Taps Provide Both A Total Pressure Measurement Upstream Of The Venturi Contraction And A Venturi Throat Pressure Measurement, Facilitating Built-In Flow Rate Measurement And/Or Determination Of Liquid/Vapor Transition.
- 17 Mar 2022
- Eo14042 Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing. This Innovative Capability Dramatically Adds To And Extends The Advantages Of Using A Cavitating Venturi To Isolate Combustion Chambers Or Other Downstream Process Fluctuations From Upstream Feed Pressure Conditions. This Design Will Greatly Simplify Propulsion Testing And Reduce Costs For Cases Where Desired Liquid Flow Conditions Are Either Not Precisely Understood Or Cover A Range Of High-Precision Flow Rates. The Proposed Geometry Is Capable Of Scaling To Both Ultra-High Pressure And High Flow Rate Applications. The Primary Innovation Consists Of A Unique Floating Pintle Design And Associated Structural Support With Built-In Pressure Taps. These Printed-In Pressure Taps Provide Both A Total Pressure Measurement Upstream Of The Venturi Contraction And A Venturi Throat Pressure Measurement, Facilitating Built-In Flow Rate Measurement And/Or Determination Of Liquid/Vapor Transition.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,980.00
- National Aeronautics And Space Administration (Nasa)
- FA864919PA450
- Advanced, Economical, In-Space Hybrid Propulsion
- 7 Aug 2019
- Advanced, Economical, In-Space Hybrid Propulsion
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $49,965.00
- Department Of Defense (Dod)
- 80NSSC20C0623
- High-Density, Non-Toxic, Low-Cost, Hybrid Stage For Lunar Injection
- 31 Aug 2020
- High-Density, Non-Toxic, Low-Cost, Hybrid Stage For Lunar Injection
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,647.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0381
- Wireless Field-Ready Transducer Acquisition Device
- 6 May 2021
- Wireless Field-Ready Transducer Acquisition Device
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,760.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0117
- Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing. This Innovative Capability Dramatically Adds To And Extends The Advantages Of Using A Cavitating Venturi To Isolate Combustion Chambers Or Other Downstream Process Fluctuations From Upstream Feed Pressure Conditions. This Design Will Greatly Simplify Propulsion Testing And Reduce Costs For Cases Where Desired Liquid Flow Conditions Are Either Not Precisely Understood Or Cover A Range Of High-Precision Flow Rates. The Proposed Geometry Is Capable Of Scaling To Both Ultra-High Pressure And High Flow Rate Applications. The Primary Innovation Consists Of A Unique Floating Pintle Design And Associated Structural Support With Built-In Pressure Taps. These Printed-In Pressure Taps Provide Both A Total Pressure Measurement Upstream Of The Venturi Contraction And A Venturi Throat Pressure Measurement, Facilitating Built-In Flow Rate Measurement And/Or Determination Of Liquid/Vapor Transition.
- 14 Jun 2021
- Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing. This Innovative Capability Dramatically Adds To And Extends The Advantages Of Using A Cavitating Venturi To Isolate Combustion Chambers Or Other Downstream Process Fluctuations From Upstream Feed Pressure Conditions. This Design Will Greatly Simplify Propulsion Testing And Reduce Costs For Cases Where Desired Liquid Flow Conditions Are Either Not Precisely Understood Or Cover A Range Of High-Precision Flow Rates. The Proposed Geometry Is Capable Of Scaling To Both Ultra-High Pressure And High Flow Rate Applications. The Primary Innovation Consists Of A Unique Floating Pintle Design And Associated Structural Support With Built-In Pressure Taps. These Printed-In Pressure Taps Provide Both A Total Pressure Measurement Upstream Of The Venturi Contraction And A Venturi Throat Pressure Measurement, Facilitating Built-In Flow Rate Measurement And/Or Determination Of Liquid/Vapor Transition.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,980.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC23PB530
- Sbir Phase Ii Low Cost Hybrid Rocket Orbital Transfer Stage
- 13 Jul 2023
- Sbir Phase Ii Low Cost Hybrid Rocket Orbital Transfer Stage
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $156,476.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0117
- Eo14042 Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing.
- 11 Oct 2021
- Eo14042 Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,980.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0117
- Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing. This Innovative Capability Dramatically Adds To And Extends The Advantages Of Using A Cavitating Venturi To Isolate Combustion Chambers Or Other Downstream Process Fluctuations From Upstream Feed Pressure Conditions. This Design Will Greatly Simplify Propulsion Testing And Reduce Costs For Cases Where Desired Liquid Flow Conditions Are Either Not Precisely Understood Or Cover A Range Of High-Precision Flow Rates. The Proposed Geometry Is Capable Of Scaling To Both Ultra-High Pressure And High Flow Rate Applications. The Primary Innovation Consists Of A Unique Floating Pintle Design And Associated Structural Support With Built-In Pressure Taps. These Printed-In Pressure Taps Provide Both A Total Pressure Measurement Upstream Of The Venturi Contraction And A Venturi Throat Pressure Measurement, Facilitating Built-In Flow Rate Measurement And/Or Determination Of Liquid/Vapor Transition.
- 8 Dec 2021
- Parabilis Space Technologies Is Pleased To Propose Development Of A Novel Additively Manufactured, Dynamically-Adjustable, In-Line, Cavitating Flow-Control And Measurement Venturi For Use In Advanced Propulsion System Ground Testing. This Innovative Capability Dramatically Adds To And Extends The Advantages Of Using A Cavitating Venturi To Isolate Combustion Chambers Or Other Downstream Process Fluctuations From Upstream Feed Pressure Conditions. This Design Will Greatly Simplify Propulsion Testing And Reduce Costs For Cases Where Desired Liquid Flow Conditions Are Either Not Precisely Understood Or Cover A Range Of High-Precision Flow Rates. The Proposed Geometry Is Capable Of Scaling To Both Ultra-High Pressure And High Flow Rate Applications. The Primary Innovation Consists Of A Unique Floating Pintle Design And Associated Structural Support With Built-In Pressure Taps. These Printed-In Pressure Taps Provide Both A Total Pressure Measurement Upstream Of The Venturi Contraction And A Venturi Throat Pressure Measurement, Facilitating Built-In Flow Rate Measurement And/Or Determination Of Liquid/Vapor Transition.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,980.00
- National Aeronautics And Space Administration (Nasa)