Ad Astra Rocket Co
CAGE Code: 430X5
NCAGE Code: 430X5
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 199033569
Summary
Ad Astra Rocket Co is an Active Commercial Supplier with the Cage Code 430X5 and is tracked by Dun & Bradstreet under DUNS Number 199033569..
Address
141 W Bay Area Blvd
Webster TX 77598-4111
United States
Points of Contact
No Points of Contact...
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Frequently Asked Questions (FAQ) for CAGE 430X5
- What is CAGE Code 430X5?
- 430X5 is the unique identifier used by NATO Organizations to reference the physical entity known as Ad Astra Rocket Co located at 141 W Bay Area Blvd, Webster TX 77598-4111, United States.
- Who is CAGE Code 430X5?
- 430X5 refers to Ad Astra Rocket Co located at 141 W Bay Area Blvd, Webster TX 77598-4111, United States.
- Where is CAGE Code 430X5 Located?
- CAGE Code 430X5 is located in Webster, TX, USA.
Contracting History for CAGE 430X5 Most Recent 25 Records
- 80NSSC23PB293
- Sbir Phase I: Improved Design Of The Vasimr Radio Frequency Transmission Line
- 26 Jul 2023
- Sbir Phase I: Improved Design Of The Vasimr Radio Frequency Transmission Line
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $149,951.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC23CA059
- Fy23 Sbir Phase Ii - Improved Thermo- Mechanical Design Of The Vasimr Rf Coupler
- 22 May 2023
- Fy23 Sbir Phase Ii - Improved Thermo- Mechanical Design Of The Vasimr Rf Coupler
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $848,798.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC23CA059
- Fy23 Sbir Phase Ii - Improved Thermo- Mechanical Design Of The Vasimr Rf Coupler
- 30 May 2023
- Fy23 Sbir Phase Ii - Improved Thermo- Mechanical Design Of The Vasimr Rf Coupler
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $848,798.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC22PA916
- Eo14042 Sbir Phase I Improved Thermo-Mechanical Design Of The Vasimr Rf Coupler
- 21 Jul 2022
- Eo14042 Sbir Phase I Improved Thermo-Mechanical Design Of The Vasimr Rf Coupler
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $149,999.00
- National Aeronautics And Space Administration (Nasa)
- NNH15CN86C
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- 7 Mar 2023
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- Nasa Headquarters
- National Aeronautics And Space Administration (Nasa)
- $8,868,091.00
- National Aeronautics And Space Administration (Nasa)
- NNH15CN86C
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- 28 Oct 2020
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- Nasa Headquarters
- National Aeronautics And Space Administration (Nasa)
- $9,060,564.00
- National Aeronautics And Space Administration (Nasa)
- NNH15CN86C
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- 4 Jan 2021
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- Nasa Headquarters
- National Aeronautics And Space Administration (Nasa)
- $9,060,564.00
- National Aeronautics And Space Administration (Nasa)
- NNH15CN86C
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- 17 Dec 2020
- Nasa Broad Agency Announcement Award Nnh15zcq001k. The Objectives Of This Work Are To Demonstrate And Measure Key Technical Functions And Parameters Relevant To Nasa. Ad Astras Well Demonstrated Experimental And Engineering Development Practices Will Be Followed Throughout The Project. Ad Astra Will Demonstrate The Following Power. Ad Astra Will Perform Operational Thermal Steady State Tests In A Design That Is Efficient And Extensible To Continuous Operations Per Thruster. Trl 5 Ppus. Ad Astra Will Use Existing Trl5 Radio Frequency Generators (Rf Ppus) That Were Developed And Built By Nautel Ltd And Proven In Vx 200 Testing. These Ppus Are Rated For Steady State Operation, Have Already Demonstrated A Combined Efficiency Percentage And A Specific Mass. Lifetime. Ad Astra Will Carry Out 100 Hours Continuous Lifetime Testing For The Full 100 Hours At Full Thermal Steady State. Ad Astra Will Perform Erosion Measurements At The End Of The Test With A Precision Goal Sufficient To Extrapolate Operational (Thrusting) Lifetime To A Number Of Hours. Performance. Ad Astra Will Measure Rocket Performance Using Vx 200 Peer Reviewed Published Techniques In Each Phase Of The Project. Performance Measurements Made During Long Duration Steady State Operations Drive Cost. Excluding The Laboratory Superconducting Magnet Cooling Power, Ad Astra Will Verify A System Efficiency Goal Of Greater Than 60 Percent, Including The Rf Ppus, At A Specific Impulse Of Interest Using Argon Propellant. Ad Astra Will Also Carry Out Variable Specific Impulse Testing Within A Range. These Tests Will Allow Trl 6 Designs That Will Achieve Total System Efficiency Greater Than 60 Percent In The Specific Impulse Range Of 2000 S To 5000 S Using High Temperature Superconductors With Argon And Krypton Propellants.
- Nasa Goddard Space Flight Center
- National Aeronautics And Space Administration (Nasa)
- $9,060,564.00
- National Aeronautics And Space Administration (Nasa)