Launchpoint Technologies, Inc.
Dba Magnetic Moments
CAGE Code: 098Q6
NCAGE Code: 098Q6
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 826728685
Summary
Launchpoint Technologies, Inc., Dba Magnetic Moments is an Active Commercial Supplier with the Cage Code 098Q6 and is tracked by Dun & Bradstreet under DUNS Number 826728685..
Address
5735 Hollister Ave Ste B
Goleta CA 93117-6410
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 098Q6
- What is CAGE Code 098Q6?
- 098Q6 is the unique identifier used by NATO Organizations to reference the physical entity known as Launchpoint Technologies, Inc. Dba Magnetic Moments located at 5735 Hollister Ave Ste B, Goleta CA 93117-6410, United States.
- Who is CAGE Code 098Q6?
- 098Q6 refers to Launchpoint Technologies, Inc. Dba Magnetic Moments located at 5735 Hollister Ave Ste B, Goleta CA 93117-6410, United States.
- Where is CAGE Code 098Q6 Located?
- CAGE Code 098Q6 is located in Goleta, CA, USA.
Contracting History for CAGE 098Q6 Most Recent 25 Records
- FA864921P0250
- Development, Systems Integration, And Flight Testing Of An 80 Kilowatt Hybrid Electric Aircraft Propulsion System
- 3 Dec 2020
- Development, Systems Integration, And Flight Testing Of An 80 Kilowatt Hybrid Electric Aircraft Propulsion System
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $149,932.00
- Department Of Defense (Dod)
- FA864921P0240
- Reliable And Lightweight Polyphase Motor And Drive Solutions For Electric Vertical Take Off And Landing Propulsion
- 3 Dec 2020
- Reliable And Lightweight Polyphase Motor And Drive Solutions For Electric Vertical Take Off And Landing Propulsion
- Fa8649 Usaf Sbir Sttr Contracting
- Department Of Defense (Dod)
- $149,990.00
- Department Of Defense (Dod)
- NNC17CA03C
- Igf::Ot::Igf Administration
- 12 Jun 2017
- Igf::Ot::Igf Administration
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P1894
- This Sbir Phase I Develops Hardware And Software For Energy Management In Electric Vtol Aircraft. It Focuses On Techniques To Ensure Short-Time-Scale Stability In Power Micro-Grids, And Optimization-Based Control At Somewhat Longer (~10-100 Ms) Time-Scales For Propulsion System And Vehicle Control, Which Is Managed By A Vehicle Energy Management System (Vems). Fast Optimization And Model-Based Decision Making Are Key To The Approach. Experiments Will Be Conducted With A Hybrid Power Plant Consisting Of An Internal Combustion Engine, An Iron-Less Dual-Halbach-Array Starter Motor/Generator, And A New 6-Phase Regenerative Motor Drive. The Project Is Organized Into Three Technical Objectives: To #1: Reconfi Gurable Component, Subsystem, And System Topology Models Reconfigurability Is Enabled At Three Levels In The Vems-Controlled System. At The Component Level, Parametric Models Are Used So That Components In A New Vehicle System Or A Faulted System Can Be Configured With A Parameter List. Subsystems Are Similarly Configured. At The System Level, The Topology Is Reconfigurable Because Of Technical Conditions (Incremental Passivity) Placed On Each Component To Ensure That The Assembled Micro-Grid Is Stable Regardless Of The Interconnection. With Stable Short-Time-Scale Dynamics, The Vems Uses Component Models To Optimally Manage Interactions On The Micro-Grid. To #2: Incremental Passivity With Application To A 1.5Kw Regenerative Drive Launchpoint Proposes To Design A 1.5Kw Regenerative Drive For The 6-Phase Starter Motor/Generator Such That It Is Incrementally Passive As Seen From The Bus. To #3: Real-Time Optimal Control For Energy Management The Project Will Make Use Of A Recently Developed Tool, Named Tenscalc, That Generates Specialized C-Code For Real-Time Decision And Control With Up To A Few Thousand Optimization Variables/Constraints. This Fast Optimization Tool Will Be At The Heart Of The Vems System And Enable Millisecond Time-Scale Decision Making.
- 12 Feb 2019
- This Sbir Phase I Develops Hardware And Software For Energy Management In Electric Vtol Aircraft. It Focuses On Techniques To Ensure Short-Time-Scale Stability In Power Micro-Grids, And Optimization-Based Control At Somewhat Longer (~10-100 Ms) Time-Scales For Propulsion System And Vehicle Control, Which Is Managed By A Vehicle Energy Management System (Vems). Fast Optimization And Model-Based Decision Making Are Key To The Approach. Experiments Will Be Conducted With A Hybrid Power Plant Consisting Of An Internal Combustion Engine, An Iron-Less Dual-Halbach-Array Starter Motor/Generator, And A New 6-Phase Regenerative Motor Drive. The Project Is Organized Into Three Technical Objectives: To #1: Reconfi Gurable Component, Subsystem, And System Topology Models Reconfigurability Is Enabled At Three Levels In The Vems-Controlled System. At The Component Level, Parametric Models Are Used So That Components In A New Vehicle System Or A Faulted System Can Be Configured With A Parameter List. Subsystems Are Similarly Configured. At The System Level, The Topology Is Reconfigurable Because Of Technical Conditions (Incremental Passivity) Placed On Each Component To Ensure That The Assembled Micro-Grid Is Stable Regardless Of The Interconnection. With Stable Short-Time-Scale Dynamics, The Vems Uses Component Models To Optimally Manage Interactions On The Micro-Grid. To #2: Incremental Passivity With Application To A 1.5Kw Regenerative Drive Launchpoint Proposes To Design A 1.5Kw Regenerative Drive For The 6-Phase Starter Motor/Generator Such That It Is Incrementally Passive As Seen From The Bus. To #3: Real-Time Optimal Control For Energy Management The Project Will Make Use Of A Recently Developed Tool, Named Tenscalc, That Generates Specialized C-Code For Real-Time Decision And Control With Up To A Few Thousand Optimization Variables/Constraints. This Fast Optimization Tool Will Be At The Heart Of The Vems System And Enable Millisecond Time-Scale Decision Making.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,970.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2894
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- 26 Nov 2019
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $71,889.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Other Administrative Action. Option To Extend The Term Of The Contract.
- 4 Oct 2018
- Other Administrative Action. Option To Extend The Term Of The Contract.
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- N6833517C0298
- Research And Development Igf::Ot::Igf
- 12 Apr 2017
- Research And Development Igf::Ot::Igf
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $124,977.00
- Department Of Defense (Dod)
- 80NSSC17P0571
- Electronic Speed Controller
- 29 Mar 2018
- Electronic Speed Controller
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $20,000.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Award For Design Of An Innovative Compact Additively Manufactured Electric Motor
- 5 Apr 2019
- Award For Design Of An Innovative Compact Additively Manufactured Electric Motor
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Design Of An Innovative Compact Additively Manufactured Electric Motor. Electric Motors (Electric Machines) Are Being Proposed And Developed For Nasa Aeronautics Programs For All Electric And Hybrid Electric Aircraft Applications. The Use Of Electric Motors In Conjunction With Efficient Power Supplies Offers Significant Reductions In Emissions And Fuel Burn Compared To Turbine Engine Propulsion. The Key To The Wider Utilization Of Electric Motors Is That They Be Compact And Lightweight With Power Densities And Efficiencies That Are Much Higher Than The Current State Of The Art. New Manufacturing Methods Are Needed To Obtain Innovative Motor Designs That Have The Necessary Power Densities. Additive Manufacturing Offers The Potential To Radically Change The Motor So That They Have Compact Designs, Multi Material Components, Innovative Cooling, And Optimally Designed And Manufactured Components. The Nasa Convergent Aeronautics Solutions Project Is Supporting An Effort Entitled Compact Additively Manufactured Innovative Electric Motor (Camiem). Advanced Electric Motors With Innovative Designs And High Power Densities Will Be Developed. The Overall Team Will Consists Of Nasa Aeronautics Centers, A Private Company, And A University. The Team Will Work Collectively To Identify Design Improvements That Can Be Enabled By Additive Manufacturing Technologies. Additive Manufacturing Technologies Will Be Optimized And Applied Toward Improving The Performance Of Sub Elements And Components. System Studies Will Be Conducted To Determine Aircraft Mission Benefits From Electric Motor Designs Which Are Lightweight, High Power Dense, And Efficient. Baseline Motors Which Utilize Conventional Manufacturing Methods Will Be Built And Tested. A New Motor, Which Utilizes Additive Manufacturing For The Various Motor Components Will Also Be Built And Tested And Performance Gains Will Be Evaluated.
- 15 Oct 2019
- Design Of An Innovative Compact Additively Manufactured Electric Motor. Electric Motors (Electric Machines) Are Being Proposed And Developed For Nasa Aeronautics Programs For All Electric And Hybrid Electric Aircraft Applications. The Use Of Electric Motors In Conjunction With Efficient Power Supplies Offers Significant Reductions In Emissions And Fuel Burn Compared To Turbine Engine Propulsion. The Key To The Wider Utilization Of Electric Motors Is That They Be Compact And Lightweight With Power Densities And Efficiencies That Are Much Higher Than The Current State Of The Art. New Manufacturing Methods Are Needed To Obtain Innovative Motor Designs That Have The Necessary Power Densities. Additive Manufacturing Offers The Potential To Radically Change The Motor So That They Have Compact Designs, Multi Material Components, Innovative Cooling, And Optimally Designed And Manufactured Components. The Nasa Convergent Aeronautics Solutions Project Is Supporting An Effort Entitled Compact Additively Manufactured Innovative Electric Motor (Camiem). Advanced Electric Motors With Innovative Designs And High Power Densities Will Be Developed. The Overall Team Will Consists Of Nasa Aeronautics Centers, A Private Company, And A University. The Team Will Work Collectively To Identify Design Improvements That Can Be Enabled By Additive Manufacturing Technologies. Additive Manufacturing Technologies Will Be Optimized And Applied Toward Improving The Performance Of Sub Elements And Components. System Studies Will Be Conducted To Determine Aircraft Mission Benefits From Electric Motor Designs Which Are Lightweight, High Power Dense, And Efficient. Baseline Motors Which Utilize Conventional Manufacturing Methods Will Be Built And Tested. A New Motor, Which Utilizes Additive Manufacturing For The Various Motor Components Will Also Be Built And Tested And Performance Gains Will Be Evaluated.
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Addendum Clause To Contract
- 21 Aug 2018
- Addendum Clause To Contract
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2894
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- 2 Jul 2019
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $71,889.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Design Of Innovative Compact Additively Manufactured Electric Motor. Electric Motors (Electric Machines) Are Being Proposed And Developed For Nasa Aeronautics Programs For All Electric And Hybrid Electric Aircraft Applications. The Use Of Electric Motors In Conjunction With Efficient Power Supplies Offers Significant Reductions In Emissions And Fuel Burn Compared To Turbine Engine Propulsion. The Key To The Wider Utilization Of Electric Motors Is That They Be Compact And Lightweight With Power Densities And Efficiencies That Are Much Higher Than The Current State Of The Art. New Manufacturing Methods Are Needed To Obtain Innovative Motor Designs That Have The Necessary Power Densities. Additive Manufacturing Offers The Potential To Radically Change The Motor So That They Have Compact Designs, Multi Material Components, Innovative Cooling, And Optimally Designed And Manufactured Components. The Nasa Convergent Aeronautics Solutions Project Is Supporting An Effort Entitled Compact Additively Manufactured Innovative Electric Motor (Camiem). Advanced Electric Motors With Innovative Designs And High Power Densities Will Be Developed. The Overall Team Will Consists Of Nasa Aeronautics Centers, A Private Company, And A University. The Team Will Work Collectively To Identify Design Improvements That Can Be Enabled By Additive Manufacturing Technologies. Additive Manufacturing Technologies Will Be Optimized And Applied Toward Improving The Performance Of Sub Elements And Components. System Studies Will Be Conducted To Determine Aircraft Mission Benefits From Electric Motor Designs Which Are Lightweight, High Power Dense, And Efficient. Baseline Motors Which Utilize Conventional Manufacturing Methods Will Be Built And Tested. A New Motor, Which Utilizes Additive Manufacturing For The Various Motor Components Will Also Be Built And Tested And Performance Gains Will Be Evaluated.
- 15 Apr 2019
- Design Of Innovative Compact Additively Manufactured Electric Motor. Electric Motors (Electric Machines) Are Being Proposed And Developed For Nasa Aeronautics Programs For All Electric And Hybrid Electric Aircraft Applications. The Use Of Electric Motors In Conjunction With Efficient Power Supplies Offers Significant Reductions In Emissions And Fuel Burn Compared To Turbine Engine Propulsion. The Key To The Wider Utilization Of Electric Motors Is That They Be Compact And Lightweight With Power Densities And Efficiencies That Are Much Higher Than The Current State Of The Art. New Manufacturing Methods Are Needed To Obtain Innovative Motor Designs That Have The Necessary Power Densities. Additive Manufacturing Offers The Potential To Radically Change The Motor So That They Have Compact Designs, Multi Material Components, Innovative Cooling, And Optimally Designed And Manufactured Components. The Nasa Convergent Aeronautics Solutions Project Is Supporting An Effort Entitled Compact Additively Manufactured Innovative Electric Motor (Camiem). Advanced Electric Motors With Innovative Designs And High Power Densities Will Be Developed. The Overall Team Will Consists Of Nasa Aeronautics Centers, A Private Company, And A University. The Team Will Work Collectively To Identify Design Improvements That Can Be Enabled By Additive Manufacturing Technologies. Additive Manufacturing Technologies Will Be Optimized And Applied Toward Improving The Performance Of Sub Elements And Components. System Studies Will Be Conducted To Determine Aircraft Mission Benefits From Electric Motor Designs Which Are Lightweight, High Power Dense, And Efficient. Baseline Motors Which Utilize Conventional Manufacturing Methods Will Be Built And Tested. A New Motor, Which Utilizes Additive Manufacturing For The Various Motor Components Will Also Be Built And Tested And Performance Gains Will Be Evaluated.
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2894
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- 24 Sep 2018
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $71,889.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- The Use Of Electric Motors In Conjunction With Efficient Power Supplies Offers Significant Reductions In Emissions And Fuel Burn Compared To Turbine Engine Propulsion.
- 13 Feb 2019
- The Use Of Electric Motors In Conjunction With Efficient Power Supplies Offers Significant Reductions In Emissions And Fuel Burn Compared To Turbine Engine Propulsion.
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- W911QX18P0161
- 6 Month Sbir Phase I Topic A18-021 The Contractor Shall Research The Development Of Electric Machines And Hybrid Drives For Vertical Takeoff And Lauding (Vtol) Tactical Air Vehicles.
- 23 Jul 2018
- 6 Month Sbir Phase I Topic A18-021 The Contractor Shall Research The Development Of Electric Machines And Hybrid Drives For Vertical Takeoff And Lauding (Vtol) Tactical Air Vehicles.
- W6qk Acc-Apg Adelphi
- Department Of Defense (Dod)
- $149,977.29
- Department Of Defense (Dod)
- 80NSSC18P3375
- This Is For The Base Concept Of A Preliminary Functioning Draft Of Simulink Embedded Software Capable Of Being Installed In The Launchpoint Technologies 15 Kw Motor Drive/Controller.
- 14 Sep 2018
- This Is For The Base Concept Of A Preliminary Functioning Draft Of Simulink Embedded Software Capable Of Being Installed In The Launchpoint Technologies 15 Kw Motor Drive/Controller.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $15,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P1894
- This Sbir Phase I Develops Hardware And Software For Energy Management In Electric Vtol Aircraft. It Focuses On Techniques To Ensure Short-Time-Scale Stability In Power Micro-Grids, And Optimization-Based Control At Somewhat Longer (~10-100 Ms) Time-Scales For Propulsion System And Vehicle Control, Which Is Managed By A Vehicle Energy Management System (Vems). Fast Optimization And Model-Based Decision Making Are Key To The Approach. Experiments Will Be Conducted With A Hybrid Power Plant Consisting Of An Internal Combustion Engine, An Iron-Less Dual-Halbach-Array Starter Motor/Generator, And A New 6-Phase Regenerative Motor Drive. The Project Is Organized Into Three Technical Objectives: To #1: Reconfi Gurable Component, Subsystem, And System Topology Models Reconfigurability Is Enabled At Three Levels In The Vems-Controlled System. At The Component Level, Parametric Models Are Used So That Components In A New Vehicle System Or A Faulted System Can Be Configured With A Parameter List. Subsystems Are Similarly Configured. At The System Level, The Topology Is Reconfigurable Because Of Technical Conditions (Incremental Passivity) Placed On Each Component To Ensure That The Assembled Micro-Grid Is Stable Regardless Of The Interconnection. With Stable Short-Time-Scale Dynamics, The Vems Uses Component Models To Optimally Manage Interactions On The Micro-Grid. To #2: Incremental Passivity With Application To A 1.5Kw Regenerative Drive Launchpoint Proposes To Design A 1.5Kw Regenerative Drive For The 6-Phase Starter Motor/Generator Such That It Is Incrementally Passive As Seen From The Bus. To #3: Real-Time Optimal Control For Energy Management The Project Will Make Use Of A Recently Developed Tool, Named Tenscalc, That Generates Specialized C-Code For Real-Time Decision And Control With Up To A Few Thousand Optimization Variables/Constraints. This Fast Optimization Tool Will Be At The Heart Of The Vems System And Enable Millisecond Time-Scale Decision Making.
- 30 Jan 2019
- This Sbir Phase I Develops Hardware And Software For Energy Management In Electric Vtol Aircraft. It Focuses On Techniques To Ensure Short-Time-Scale Stability In Power Micro-Grids, And Optimization-Based Control At Somewhat Longer (~10-100 Ms) Time-Scales For Propulsion System And Vehicle Control, Which Is Managed By A Vehicle Energy Management System (Vems). Fast Optimization And Model-Based Decision Making Are Key To The Approach. Experiments Will Be Conducted With A Hybrid Power Plant Consisting Of An Internal Combustion Engine, An Iron-Less Dual-Halbach-Array Starter Motor/Generator, And A New 6-Phase Regenerative Motor Drive. The Project Is Organized Into Three Technical Objectives: To #1: Reconfi Gurable Component, Subsystem, And System Topology Models Reconfigurability Is Enabled At Three Levels In The Vems-Controlled System. At The Component Level, Parametric Models Are Used So That Components In A New Vehicle System Or A Faulted System Can Be Configured With A Parameter List. Subsystems Are Similarly Configured. At The System Level, The Topology Is Reconfigurable Because Of Technical Conditions (Incremental Passivity) Placed On Each Component To Ensure That The Assembled Micro-Grid Is Stable Regardless Of The Interconnection. With Stable Short-Time-Scale Dynamics, The Vems Uses Component Models To Optimally Manage Interactions On The Micro-Grid. To #2: Incremental Passivity With Application To A 1.5Kw Regenerative Drive Launchpoint Proposes To Design A 1.5Kw Regenerative Drive For The 6-Phase Starter Motor/Generator Such That It Is Incrementally Passive As Seen From The Bus. To #3: Real-Time Optimal Control For Energy Management The Project Will Make Use Of A Recently Developed Tool, Named Tenscalc, That Generates Specialized C-Code For Real-Time Decision And Control With Up To A Few Thousand Optimization Variables/Constraints. This Fast Optimization Tool Will Be At The Heart Of The Vems System And Enable Millisecond Time-Scale Decision Making.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,970.00
- National Aeronautics And Space Administration (Nasa)
- W911W618C0018
- Launch Point Sbir Phase I
- 4 Oct 2017
- Launch Point Sbir Phase I
- Acc-Aviation Applied Technology Dir
- Department Of Defense (Dod)
- $99,918.92
- Department Of Defense (Dod)
- NNC15VD10P
- Extended Period Of Performance End Date
- 25 Sep 2018
- Extended Period Of Performance End Date
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $235,000.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Igf::Ot::Igf Funding
- 11 Sep 2017
- Igf::Ot::Igf Funding
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2894
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- 15 Apr 2019
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $71,889.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P2894
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft. To Support This Capability.
- 26 Nov 2019
- The Aeromechanics Office (Code Av) At Nasa Ames Is Developing A New Capability To Test Small-Scale (Up To 24-In Diameter) Rotors To Enable Research On New Types Of Vertical Takeoff And Landing (Vtol) Aircraft. To Support This Capability.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $71,889.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P1894
- This Sbir Phase I Develops Hardware And Software For Energy Management In Electric Vtol Aircraft. It Focuses On Techniques To Ensure Short-Time-Scale Stability In Power Micro-Grids, And Optimization-Based Control At Somewhat Longer (~10-100 Ms) Time-Scales For Propulsion System And Vehicle Control, Which Is Managed By A Vehicle Energy Management System (Vems). Fast Optimization And Model-Based Decision Making Are Key To The Approach. Experiments Will Be Conducted With A Hybrid Power Plant Consisting Of An Internal Combustion Engine, An Iron-Less Dual-Halbach-Array Starter Motor/Generator, And A New 6-Phase Regenerative Motor Drive. The Project Is Organized Into Three Technical Objectives: To #1: Reconfi Gurable Component, Subsystem, And System Topology Models Reconfigurability Is Enabled At Three Levels In The Vems-Controlled System. At The Component Level, Parametric Models Are Used So That Components In A New Vehicle System Or A Faulted System Can Be Configured With A Parameter List. Subsystems Are Similarly Configured. At The System Level, The Topology Is Reconfigurable Because Of Technical Conditions (Incremental Passivity) Placed On Each Component To Ensure That The Assembled Micro-Grid Is Stable Regardless Of The Interconnection. With Stable Short-Time-Scale Dynamics, The Vems Uses Component Models To Optimally Manage Interactions On The Micro-Grid. To #2: Incremental Passivity With Application To A 1.5Kw Regenerative Drive Launchpoint Proposes To Design A 1.5Kw Regenerative Drive For The 6-Phase Starter Motor/Generator Such That It Is Incrementally Passive As Seen From The Bus. To #3: Real-Time Optimal Control For Energy Management The Project Will Make Use Of A Recently Developed Tool, Named Tenscalc, That Generates Specialized C-Code For Real-Time Decision And Control With Up To A Few Thousand Optimization Variables/Constraints. This Fast Optimization Tool Will Be At The Heart Of The Vems System And Enable Millisecond Time-Scale Decision Making.
- 27 Jul 2018
- This Sbir Phase I Develops Hardware And Software For Energy Management In Electric Vtol Aircraft. It Focuses On Techniques To Ensure Short-Time-Scale Stability In Power Micro-Grids, And Optimization-Based Control At Somewhat Longer (~10-100 Ms) Time-Scales For Propulsion System And Vehicle Control, Which Is Managed By A Vehicle Energy Management System (Vems). Fast Optimization And Model-Based Decision Making Are Key To The Approach. Experiments Will Be Conducted With A Hybrid Power Plant Consisting Of An Internal Combustion Engine, An Iron-Less Dual-Halbach-Array Starter Motor/Generator, And A New 6-Phase Regenerative Motor Drive. The Project Is Organized Into Three Technical Objectives: To #1: Reconfi Gurable Component, Subsystem, And System Topology Models Reconfigurability Is Enabled At Three Levels In The Vems-Controlled System. At The Component Level, Parametric Models Are Used So That Components In A New Vehicle System Or A Faulted System Can Be Configured With A Parameter List. Subsystems Are Similarly Configured. At The System Level, The Topology Is Reconfigurable Because Of Technical Conditions (Incremental Passivity) Placed On Each Component To Ensure That The Assembled Micro-Grid Is Stable Regardless Of The Interconnection. With Stable Short-Time-Scale Dynamics, The Vems Uses Component Models To Optimally Manage Interactions On The Micro-Grid. To #2: Incremental Passivity With Application To A 1.5Kw Regenerative Drive Launchpoint Proposes To Design A 1.5Kw Regenerative Drive For The 6-Phase Starter Motor/Generator Such That It Is Incrementally Passive As Seen From The Bus. To #3: Real-Time Optimal Control For Energy Management The Project Will Make Use Of A Recently Developed Tool, Named Tenscalc, That Generates Specialized C-Code For Real-Time Decision And Control With Up To A Few Thousand Optimization Variables/Constraints. This Fast Optimization Tool Will Be At The Heart Of The Vems System And Enable Millisecond Time-Scale Decision Making.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,970.00
- National Aeronautics And Space Administration (Nasa)
- NNC17CA03C
- Igf::Ot::Igf Design Of Innovative Compact Additively Manufactured Electric Motor.
- 14 Apr 2017
- Igf::Ot::Igf Design Of Innovative Compact Additively Manufactured Electric Motor.
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $699,996.00
- National Aeronautics And Space Administration (Nasa)