Balcones Technologies Llc
CAGE Code: 4UR93
NCAGE Code: 4UR93
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 806337460
Summary
Balcones Technologies Llc is an Active Commercial Supplier with the Cage Code 4UR93 and is tracked by Dun & Bradstreet under DUNS Number 806337460..
Address
104 Alabaster Caverns Dr
Georgetown TX 78628-7228
United States
Points of Contact
No Points of Contact...
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Frequently Asked Questions (FAQ) for CAGE 4UR93
- What is CAGE Code 4UR93?
- 4UR93 is the unique identifier used by NATO Organizations to reference the physical entity known as Balcones Technologies Llc located at 104 Alabaster Caverns Dr, Georgetown TX 78628-7228, United States.
- Who is CAGE Code 4UR93?
- 4UR93 refers to Balcones Technologies Llc located at 104 Alabaster Caverns Dr, Georgetown TX 78628-7228, United States.
- Where is CAGE Code 4UR93 Located?
- CAGE Code 4UR93 is located in Georgetown, TX, USA.
Contracting History for CAGE 4UR93 Most Recent 25 Records
- 80NSSC23PB362
- Sbir Phase I - Brushless Doubly Fed Motor For Electric Aircraft Propulsion
- 7 Jul 2023
- Sbir Phase I - Brushless Doubly Fed Motor For Electric Aircraft Propulsion
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $149,957.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0627
- Low Nest Count Brushless Doubly Fed Machine For Uam Application
- 28 Sep 2021
- Low Nest Count Brushless Doubly Fed Machine For Uam Application
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $123,935.00
- National Aeronautics And Space Administration (Nasa)
- W56HZV16C0060
- Igf::Ot::Igf Phase Ii Sbir Modification To Add Scope And Funding
- 29 May 2018
- Igf::Ot::Igf Phase Ii Sbir Modification To Add Scope And Funding
- W4gg Hq Us Army Tacom
- Department Of Defense (Dod)
- $999,018.42
- Department Of Defense (Dod)
- 80NSSC18P1178
- During The Phase I&Ii Sttr Efforts, Balcones Technologies, Llc (Bt) And The University Of Texas At Austin Center For Electromechanics (Cem) Successfully Achieved All Objectives And Developed And Delivered Concept Designs For Controlled Canfield Joint Systems (Cjs) For Numerous Applications That Currently Employ Two-Axis Gimbal Systems, Including Flywheel Energy Storage Systems, Integrated Flywheel Energy Storage And Attitude Control Systems, Controlled Moment Gyros (Cmg), And Pointing Systems For Satellite-To-Earth And Satellite-To-Satellite Space Optical Communications (Soc). While All Applications Offered Advantages For Cjs Compared To Gimbal Alternatives, A Major Result Was That The Highest Payoff Phase Ii Demonstration For Nasa And Other Commercial Applications Would Focus On A Cjs Simultaneously Sized For Two Applications: Small Satellite Cmg And Small Satellite Optical Communications. Since The Soc Application Is More Demanding And This Emerging Application Offered More Terrestrial And Space Applications, This Application Served As The Demonstration Target For Phase Ii And Beyond. Some Key Cjs-Soc Features Include: More Than 30% Improvement In Pointing Accuracy And Precision Compared To 2 Axis Gimbal Systems; Integrated Vibration Isolation System To Meet Deep Space Optical Communication Systems; Also Sized For Small Cmg Application; Wide Field Of Regard; Scalable To Large Flywheel Applications; Maximum Use Of Cots Components; Exploits Team Core Capabilities In Vibration Isolation Systems And High Precision, High Accuracy Point Systems.
- 18 Jun 2018
- During The Phase I&Ii Sttr Efforts, Balcones Technologies, Llc (Bt) And The University Of Texas At Austin Center For Electromechanics (Cem) Successfully Achieved All Objectives And Developed And Delivered Concept Designs For Controlled Canfield Joint Systems (Cjs) For Numerous Applications That Currently Employ Two-Axis Gimbal Systems, Including Flywheel Energy Storage Systems, Integrated Flywheel Energy Storage And Attitude Control Systems, Controlled Moment Gyros (Cmg), And Pointing Systems For Satellite-To-Earth And Satellite-To-Satellite Space Optical Communications (Soc). While All Applications Offered Advantages For Cjs Compared To Gimbal Alternatives, A Major Result Was That The Highest Payoff Phase Ii Demonstration For Nasa And Other Commercial Applications Would Focus On A Cjs Simultaneously Sized For Two Applications: Small Satellite Cmg And Small Satellite Optical Communications. Since The Soc Application Is More Demanding And This Emerging Application Offered More Terrestrial And Space Applications, This Application Served As The Demonstration Target For Phase Ii And Beyond. Some Key Cjs-Soc Features Include: More Than 30% Improvement In Pointing Accuracy And Precision Compared To 2 Axis Gimbal Systems; Integrated Vibration Isolation System To Meet Deep Space Optical Communication Systems; Also Sized For Small Cmg Application; Wide Field Of Regard; Scalable To Large Flywheel Applications; Maximum Use Of Cots Components; Exploits Team Core Capabilities In Vibration Isolation Systems And High Precision, High Accuracy Point Systems.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $19,994.00
- National Aeronautics And Space Administration (Nasa)
- N6833521C0664
- Correct Delivery Dates To Reflect Award Date Of 7/26/21.
- 1 Sep 2021
- Correct Delivery Dates To Reflect Award Date Of 7/26/21.
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $140,000.00
- Department Of Defense (Dod)
- W56HZV16C0060
- Contract Modification To Extend Period Of Performance By Six Weeks.
- 31 Oct 2018
- Contract Modification To Extend Period Of Performance By Six Weeks.
- W4gg Hq Us Army Tacom
- Department Of Defense (Dod)
- $999,018.42
- Department Of Defense (Dod)
- N6833521C0664
- Research And Development.
- 25 Jul 2021
- Research And Development.
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $140,000.00
- Department Of Defense (Dod)
- 80NSSC17C0032
- During Our Phase I Sttr Effort, Balcones Technologies, Llc And The University Of Texas Center For Electromechanics Successfully Achieved All Phase I Objectives And Developed An Advanced Concept For Mega- Watt (Mw) Class, High Voltage, Variable Frequency, Aircraft Electric Propulsor Motors. Our Concept Exploits Doubly Fed Generator Technology That Has Received Considerable Development For Wind Energy Applications And Adapts It To The Aircraft Electric Propulsor Application. In Particular, The Wind Application Is Low Frequency, Low Speed, 600V, Fixed Frequency, Mw Class, Slip-Ring Or Brushless Doubly Fed Generator Technology. Our Proposed Effort Adapts That Technology To Develop Higher Voltage (1Kv), Variable Frequency, High Speed Aircraft Electric Brushless Doubly Fed Motors (Bdfm) For The Advanced Propulsor Application. Important Advantages Of Our Propulsor Technical Solution, Our Team And Our Program Plan Are: 1. Our Dual Fed Motor Concept Is Brushless, Which Was Identified As Highly Important By Aircraft Oem/Integrators When Briefed On Our Approach. 2. Our Bdfm Propulsor Motor Results In A 40% Reduction In Mass Of The Propulsor Unit (Motor, Converter, And Gear System) Compared To Other Approaches (Including Permanent Magnet Propulsors) And Also Increases Propulsor Unit Efficiency By 4%. 3. Our Bdfm Propulsor Motor Approach Is Feasible And Viable Because Of Its Roots In Doubly Fed Generators For Wind Energy Applications, But It Also Represents An Advancement In The State Of The Art For Brushless Doubly Fed Machines And Advancement In The State-Of-The-Art For Electric Propulsor Units. 4. Our Team Is Highly Qualified To Succeed In Our Proposed Effort With World Class Subject Matter Experts In The Key Aspects Of Our Bdfm Propulsor Motor. 5. Our Commercialization Plan And Transition To Production Plan Sets The Seeds For Long Term Success By Bringing On A Future Manufacturer As A Strategic Partner During Our Phase Ii Effort.
- 29 Oct 2019
- During Our Phase I Sttr Effort, Balcones Technologies, Llc And The University Of Texas Center For Electromechanics Successfully Achieved All Phase I Objectives And Developed An Advanced Concept For Mega- Watt (Mw) Class, High Voltage, Variable Frequency, Aircraft Electric Propulsor Motors. Our Concept Exploits Doubly Fed Generator Technology That Has Received Considerable Development For Wind Energy Applications And Adapts It To The Aircraft Electric Propulsor Application. In Particular, The Wind Application Is Low Frequency, Low Speed, 600V, Fixed Frequency, Mw Class, Slip-Ring Or Brushless Doubly Fed Generator Technology. Our Proposed Effort Adapts That Technology To Develop Higher Voltage (1Kv), Variable Frequency, High Speed Aircraft Electric Brushless Doubly Fed Motors (Bdfm) For The Advanced Propulsor Application. Important Advantages Of Our Propulsor Technical Solution, Our Team And Our Program Plan Are: 1. Our Dual Fed Motor Concept Is Brushless, Which Was Identified As Highly Important By Aircraft Oem/Integrators When Briefed On Our Approach. 2. Our Bdfm Propulsor Motor Results In A 40% Reduction In Mass Of The Propulsor Unit (Motor, Converter, And Gear System) Compared To Other Approaches (Including Permanent Magnet Propulsors) And Also Increases Propulsor Unit Efficiency By 4%. 3. Our Bdfm Propulsor Motor Approach Is Feasible And Viable Because Of Its Roots In Doubly Fed Generators For Wind Energy Applications, But It Also Represents An Advancement In The State Of The Art For Brushless Doubly Fed Machines And Advancement In The State-Of-The-Art For Electric Propulsor Units. 4. Our Team Is Highly Qualified To Succeed In Our Proposed Effort With World Class Subject Matter Experts In The Key Aspects Of Our Bdfm Propulsor Motor. 5. Our Commercialization Plan And Transition To Production Plan Sets The Seeds For Long Term Success By Bringing On A Future Manufacturer As A Strategic Partner During Our Phase Ii Effort.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,781.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC17C0032
- During Our Phase I Sttr Effort, Balcones Technologies, Llc And The University Of Texas Center For Electromechanics Successfully Achieved All Phase I Objectives And Developed An Advanced Concept For Mega- Watt (Mw) Class, High Voltage, Variable Frequency, Aircraft Electric Propulsor Motors. Our Concept Exploits Doubly Fed Generator Technology That Has Received Considerable Development For Wind Energy Applications And Adapts It To The Aircraft Electric Propulsor Application. In Particular, The Wind Application Is Low Frequency, Low Speed, 600V, Fixed Frequency, Mw Class, Slip-Ring Or Brushless Doubly Fed Generator Technology. Our Proposed Effort Adapts That Technology To Develop Higher Voltage (1Kv), Variable Frequency, High Speed Aircraft Electric Brushless Doubly Fed Motors (Bdfm) For The Advanced Propulsor Application. Important Advantages Of Our Propulsor Technical Solution, Our Team And Our Program Plan Are: 1. Our Dual Fed Motor Concept Is Brushless, Which Was Identified As Highly Important By Aircraft Oem/Integrators When Briefed On Our Approach. 2. Our Bdfm Propulsor Motor Results In A 40% Reduction In Mass Of The Propulsor Unit (Motor, Converter, And Gear System) Compared To Other Approaches (Including Permanent Magnet Propulsors) And Also Increases Propulsor Unit Efficiency By 4%. 3. Our Bdfm Propulsor Motor Approach Is Feasible And Viable Because Of Its Roots In Doubly Fed Generators For Wind Energy Applications, But It Also Represents An Advancement In The State Of The Art For Brushless Doubly Fed Machines And Advancement In The State-Of-The-Art For Electric Propulsor Units. 4. Our Team Is Highly Qualified To Succeed In Our Proposed Effort With World Class Subject Matter Experts In The Key Aspects Of Our Bdfm Propulsor Motor. 5. Our Commercialization Plan And Transition To Production Plan Sets The Seeds For Long Term Success By Bringing On A Future Manufacturer As A Strategic Partner During Our Phase Ii Effort.
- 4 Jun 2018
- During Our Phase I Sttr Effort, Balcones Technologies, Llc And The University Of Texas Center For Electromechanics Successfully Achieved All Phase I Objectives And Developed An Advanced Concept For Mega- Watt (Mw) Class, High Voltage, Variable Frequency, Aircraft Electric Propulsor Motors. Our Concept Exploits Doubly Fed Generator Technology That Has Received Considerable Development For Wind Energy Applications And Adapts It To The Aircraft Electric Propulsor Application. In Particular, The Wind Application Is Low Frequency, Low Speed, 600V, Fixed Frequency, Mw Class, Slip-Ring Or Brushless Doubly Fed Generator Technology. Our Proposed Effort Adapts That Technology To Develop Higher Voltage (1Kv), Variable Frequency, High Speed Aircraft Electric Brushless Doubly Fed Motors (Bdfm) For The Advanced Propulsor Application. Important Advantages Of Our Propulsor Technical Solution, Our Team And Our Program Plan Are: 1. Our Dual Fed Motor Concept Is Brushless, Which Was Identified As Highly Important By Aircraft Oem/Integrators When Briefed On Our Approach. 2. Our Bdfm Propulsor Motor Results In A 40% Reduction In Mass Of The Propulsor Unit (Motor, Converter, And Gear System) Compared To Other Approaches (Including Permanent Magnet Propulsors) And Also Increases Propulsor Unit Efficiency By 4%. 3. Our Bdfm Propulsor Motor Approach Is Feasible And Viable Because Of Its Roots In Doubly Fed Generators For Wind Energy Applications, But It Also Represents An Advancement In The State Of The Art For Brushless Doubly Fed Machines And Advancement In The State-Of-The-Art For Electric Propulsor Units. 4. Our Team Is Highly Qualified To Succeed In Our Proposed Effort With World Class Subject Matter Experts In The Key Aspects Of Our Bdfm Propulsor Motor. 5. Our Commercialization Plan And Transition To Production Plan Sets The Seeds For Long Term Success By Bringing On A Future Manufacturer As A Strategic Partner During Our Phase Ii Effort.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,781.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0062
- Bdfm Development Program
- 12 Nov 2020
- Bdfm Development Program
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $84,334.00
- National Aeronautics And Space Administration (Nasa)
- W56HZV16C0060
- Contract Modification To Transfer Contractor Acquired Property To Tardec.
- 21 Dec 2018
- Contract Modification To Transfer Contractor Acquired Property To Tardec.
- W4gg Hq Us Army Tacom
- Department Of Defense (Dod)
- $999,018.42
- Department Of Defense (Dod)
- W56HZV16C0060
- Modification P00005 To Remove $25,990.00 From Subclin 0002Aa That Was Erroneously Added By Padds On Mod P00004.
- 31 Dec 2018
- Modification P00005 To Remove $25,990.00 From Subclin 0002Aa That Was Erroneously Added By Padds On Mod P00004.
- W4gg Hq Us Army Tacom
- Department Of Defense (Dod)
- $999,018.42
- Department Of Defense (Dod)
- 80NSSC20C0062
- Bdfm Development Program
- 16 Sep 2021
- Bdfm Development Program
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $84,334.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0062
- Balcones Technologies
- 5 Jun 2020
- Balcones Technologies
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $84,344.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0627
- Eo14042 Low Nest Count Brushless Doubly Fed Machine (Bdfm) For Uam Application
- 22 Sep 2022
- Eo14042 Low Nest Count Brushless Doubly Fed Machine (Bdfm) For Uam Application
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $123,935.00
- National Aeronautics And Space Administration (Nasa)
- W56HZV16C0060
- Contract Modification To Transfer Contractor Acquired Property To Tardec.
- 5 Mar 2020
- Contract Modification To Transfer Contractor Acquired Property To Tardec.
- Dcma Dallas
- Department Of Defense (Dod)
- $988,025.88
- Department Of Defense (Dod)
- N6833519C0737
- Progress Report
- 23 Sep 2019
- Progress Report
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $139,920.00
- Department Of Defense (Dod)
- 80NSSC20C0062
- Bdfm Development Program
- 24 Apr 2020
- Bdfm Development Program
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $84,334.00
- National Aeronautics And Space Administration (Nasa)
- N6893620C0052
- Sbir Phase 1 Topic N193-146 Contract Award
- 19 Feb 2020
- Sbir Phase 1 Topic N193-146 Contract Award
- Naval Air Warfare Center
- Department Of Defense (Dod)
- $139,830.18
- Department Of Defense (Dod)
- 80NSSC20C0062
- Brushless Doubly Fed Machine (Bdfm) Development For Urban Air Mobility
- 19 May 2020
- Brushless Doubly Fed Machine (Bdfm) Development For Urban Air Mobility
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $84,334.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC17C0032
- Brushless Doubly Fed Motor For Mega-Watt Class Propulsor Power Unit
- 9 Mar 2020
- Brushless Doubly Fed Motor For Mega-Watt Class Propulsor Power Unit
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,781.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC17P0298
- To These Ends, Balcones Technology S Expertise Is Requested To Assist Specifically In The Area Of Research And Development Of Control Structure For Closed-Loop Actuation, With An End Goal To Demonstrate Full Closed Loop Cjs Control With Realistic Trajectories In Laboratory Using Iroc Payload Model. In Addition, Balcones Technology Shall Provide A Cjs Simulation Model To Nasa For The Prediction Of Spacecraft Vibrational Propagation Through Cjs, Which Will Also Be Empirically Verified In The Laboratory By The Nasa Team. Finally, Balcones Technology Will Investigate Future Options To Modify System For Further 1G Testing, Examine Other Potential Applications And Implementations Of The Cjs Technology To Make Recommendations For Future Iterations Of The Technology, And Prepare Necessary Reporting And Publishing For Scan Technology Reviews.
- 18 Jun 2018
- To These Ends, Balcones Technology S Expertise Is Requested To Assist Specifically In The Area Of Research And Development Of Control Structure For Closed-Loop Actuation, With An End Goal To Demonstrate Full Closed Loop Cjs Control With Realistic Trajectories In Laboratory Using Iroc Payload Model. In Addition, Balcones Technology Shall Provide A Cjs Simulation Model To Nasa For The Prediction Of Spacecraft Vibrational Propagation Through Cjs, Which Will Also Be Empirically Verified In The Laboratory By The Nasa Team. Finally, Balcones Technology Will Investigate Future Options To Modify System For Further 1G Testing, Examine Other Potential Applications And Implementations Of The Cjs Technology To Make Recommendations For Future Iterations Of The Technology, And Prepare Necessary Reporting And Publishing For Scan Technology Reviews.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $0.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC17C0032
- During Our Phase I Sttr Effort, Balcones Technologies, Llc And The University Of Texas Center For Electromechanics Successfully Achieved All Phase I Objectives And Developed An Advanced Concept For Mega- Watt (Mw) Class, High Voltage, Variable Frequency, Aircraft Electric Propulsor Motors. Our Concept Exploits Doubly Fed Generator Technology That Has Received Considerable Development For Wind Energy Applications And Adapts It To The Aircraft Electric Propulsor Application. In Particular, The Wind Application Is Low Frequency, Low Speed, 600V, Fixed Frequency, Mw Class, Slip-Ring Or Brushless Doubly Fed Generator Technology. Our Proposed Effort Adapts That Technology To Develop Higher Voltage (1Kv), Variable Frequency, High Speed Aircraft Electric Brushless Doubly Fed Motors (Bdfm) For The Advanced Propulsor Application. Important Advantages Of Our Propulsor Technical Solution, Our Team And Our Program Plan Are: 1. Our Dual Fed Motor Concept Is Brushless, Which Was Identified As Highly Important By Aircraft Oem/Integrators When Briefed On Our Approach. 2. Our Bdfm Propulsor Motor Results In A 40% Reduction In Mass Of The Propulsor Unit (Motor, Converter, And Gear System) Compared To Other Approaches (Including Permanent Magnet Propulsors) And Also Increases Propulsor Unit Efficiency By 4%. 3. Our Bdfm Propulsor Motor Approach Is Feasible And Viable Because Of Its Roots In Doubly Fed Generators For Wind Energy Applications, But It Also Represents An Advancement In The State Of The Art For Brushless Doubly Fed Machines And Advancement In The State-Of-The-Art For Electric Propulsor Units. 4. Our Team Is Highly Qualified To Succeed In Our Proposed Effort With World Class Subject Matter Experts In The Key Aspects Of Our Bdfm Propulsor Motor. 5. Our Commercialization Plan And Transition To Production Plan Sets The Seeds For Long Term Success By Bringing On A Future Manufacturer As A Strategic Partner During Our Phase Ii Effort.
- 19 Aug 2019
- During Our Phase I Sttr Effort, Balcones Technologies, Llc And The University Of Texas Center For Electromechanics Successfully Achieved All Phase I Objectives And Developed An Advanced Concept For Mega- Watt (Mw) Class, High Voltage, Variable Frequency, Aircraft Electric Propulsor Motors. Our Concept Exploits Doubly Fed Generator Technology That Has Received Considerable Development For Wind Energy Applications And Adapts It To The Aircraft Electric Propulsor Application. In Particular, The Wind Application Is Low Frequency, Low Speed, 600V, Fixed Frequency, Mw Class, Slip-Ring Or Brushless Doubly Fed Generator Technology. Our Proposed Effort Adapts That Technology To Develop Higher Voltage (1Kv), Variable Frequency, High Speed Aircraft Electric Brushless Doubly Fed Motors (Bdfm) For The Advanced Propulsor Application. Important Advantages Of Our Propulsor Technical Solution, Our Team And Our Program Plan Are: 1. Our Dual Fed Motor Concept Is Brushless, Which Was Identified As Highly Important By Aircraft Oem/Integrators When Briefed On Our Approach. 2. Our Bdfm Propulsor Motor Results In A 40% Reduction In Mass Of The Propulsor Unit (Motor, Converter, And Gear System) Compared To Other Approaches (Including Permanent Magnet Propulsors) And Also Increases Propulsor Unit Efficiency By 4%. 3. Our Bdfm Propulsor Motor Approach Is Feasible And Viable Because Of Its Roots In Doubly Fed Generators For Wind Energy Applications, But It Also Represents An Advancement In The State Of The Art For Brushless Doubly Fed Machines And Advancement In The State-Of-The-Art For Electric Propulsor Units. 4. Our Team Is Highly Qualified To Succeed In Our Proposed Effort With World Class Subject Matter Experts In The Key Aspects Of Our Bdfm Propulsor Motor. 5. Our Commercialization Plan And Transition To Production Plan Sets The Seeds For Long Term Success By Bringing On A Future Manufacturer As A Strategic Partner During Our Phase Ii Effort.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,781.00
- National Aeronautics And Space Administration (Nasa)