Princeton Satellite Systems Inc
CAGE Code: 1C4A9
NCAGE Code: 1C4A9
Status: Active
Type: Manufacturer
Dun & Bradstreet (DUNS): 805686870
Summary
Princeton Satellite Systems Inc is an Active Manufacturer with the Cage Code 1C4A9 and is tracked by Dun & Bradstreet under DUNS Number 805686870..
Address
6 Market St
Ste 926
Plainsboro NJ 08536-2096
United States
Points of Contact
- Telephone:
- 6092759606
- Fax:
- 6092759609
-
http://www.psatellite.com/
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Frequently Asked Questions (FAQ) for CAGE 1C4A9
- What is CAGE Code 1C4A9?
- 1C4A9 is the unique identifier used by NATO Organizations to reference the physical entity known as Princeton Satellite Systems Inc located at 6 Market St, Ste 926, Plainsboro NJ 08536-2096, United States.
- Who is CAGE Code 1C4A9?
- 1C4A9 refers to Princeton Satellite Systems Inc located at 6 Market St, Ste 926, Plainsboro NJ 08536-2096, United States.
- Where is CAGE Code 1C4A9 Located?
- CAGE Code 1C4A9 is located in Plainsboro, NJ, USA.
Contracting History for CAGE 1C4A9 Most Recent 25 Records
- HQ003422P0112
- Small Business Innovation Research Phase 1 Award For Brayton Heat Cycle Engine For Satellite Power Research
- 25 May 2023
- Small Business Innovation Research Phase 1 Award For Brayton Heat Cycle Engine For Satellite Power Research
- Washington Headquarters Services
- Department Of Defense (Dod)
- $248,055.10
- Department Of Defense (Dod)
- HQ003422P0112
- Small Business Innovation Research (Sbir) Ph 1 Study On Brayton Cycle Heat Engine For Satellite Power
- 22 Mar 2023
- Small Business Innovation Research (Sbir) Ph 1 Study On Brayton Cycle Heat Engine For Satellite Power
- Washington Headquarters Services
- Department Of Defense (Dod)
- $248,055.10
- Department Of Defense (Dod)
- HQ003422P0112
- Small Business Innovation Research (Sbir) On Brayton Cycle Heat Engine For Satellite Power
- 13 Sep 2022
- Small Business Innovation Research (Sbir) On Brayton Cycle Heat Engine For Satellite Power
- Washington Headquarters Services
- Department Of Defense (Dod)
- $248,055.10
- Department Of Defense (Dod)
- 80NSSC20C0262
- Neural Space Navigator
- 18 Sep 2020
- Neural Space Navigator
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,731.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0402
- Multi-Megawatt Superconducting Motor For Electric Aircraft
- 12 Aug 2020
- Multi-Megawatt Superconducting Motor For Electric Aircraft
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,943.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0402
- Multi-Megawatt Superconducting Motor For Electric Aircraft
- 11 Feb 2021
- Multi-Megawatt Superconducting Motor For Electric Aircraft
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,943.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0402
- Multi-Megawatt Superconducting Motor For Electric Aircraft
- 17 Sep 2020
- Multi-Megawatt Superconducting Motor For Electric Aircraft
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,943.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0262
- Neural Space Navigator
- 5 Aug 2020
- Neural Space Navigator
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,731.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0218
- This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies.
- 9 Dec 2020
- This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,981.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18P3118
- Grc Has A Need To Expand Its Scenic Simulation Toolset Capability To Generate Mission Trajectory Profiles Based On Low-Energy Transfer Methods, Through A Sbir Ph Iii Award To A Past Sbir Contract To Princeton Satellite System. Scenic Utilizes Gsfc Orbit Determination Toolbox (Odtbx) For Its Simulation Capabilities. These Capabilities Reference User-Provided Binary Spice Kernel (Bsp) Format Files Which Provide Motion/Velocity Profile Via A Lookup Functionality As A Function Of User-Selected Time. There Is A Need For Low-Energy Thrust Trajectories That Can Output Motion Profiles Using The Standard Bsp Format, So Those Motions Can Be Directly Utilized In The Existing Scenic Capabilities Without Additional Modifications. Scenic/Odtbx Uses The Latest Ephemeris Bsp Files From Jpl So Scenic Would Want The Low Energy Toolbox Capabilities To Also Utilize Those Same Gravitational Body Datasets For Consistency. Grc Would Like The Low Energy Toolbox Capability To Be Provided As Part Of The Deliverable, While Also Providing Documentation And Training To Scenic Communication System Engineers So That The Toolbox Can Be Utilized After The Completion Of The Task. Princeton Satellite Systems Will Port The Low Energy Mission Planning Toolbox (Lempt), Developed Under A Nasa Phase I Sbir
- 7 Sep 2018
- Grc Has A Need To Expand Its Scenic Simulation Toolset Capability To Generate Mission Trajectory Profiles Based On Low-Energy Transfer Methods, Through A Sbir Ph Iii Award To A Past Sbir Contract To Princeton Satellite System. Scenic Utilizes Gsfc Orbit Determination Toolbox (Odtbx) For Its Simulation Capabilities. These Capabilities Reference User-Provided Binary Spice Kernel (Bsp) Format Files Which Provide Motion/Velocity Profile Via A Lookup Functionality As A Function Of User-Selected Time. There Is A Need For Low-Energy Thrust Trajectories That Can Output Motion Profiles Using The Standard Bsp Format, So Those Motions Can Be Directly Utilized In The Existing Scenic Capabilities Without Additional Modifications. Scenic/Odtbx Uses The Latest Ephemeris Bsp Files From Jpl So Scenic Would Want The Low Energy Toolbox Capabilities To Also Utilize Those Same Gravitational Body Datasets For Consistency. Grc Would Like The Low Energy Toolbox Capability To Be Provided As Part Of The Deliverable, While Also Providing Documentation And Training To Scenic Communication System Engineers So That The Toolbox Can Be Utilized After The Completion Of The Task. Princeton Satellite Systems Will Port The Low Energy Mission Planning Toolbox (Lempt), Developed Under A Nasa Phase I Sbir
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $59,832.00
- National Aeronautics And Space Administration (Nasa)
- NNX17CM47P
- Igf::Ot::Igf High Power Nuclear Fusion Propulsion Systems Will Require High Efficiency Radio-Frequency Heating Systems In The Mhz Range For Plasma Heating. This Proposal Is For A Novel Scalable Solid State Class E Amplifier Using Silicon Carbide Switching Transistors For Plasma Heating. This System Is Potentially 100% Efficient Compared To 40% For Linear Amplifiers And Can Be Scaled To Any Desired Size By Adding Additional Segments In Parallel. The System Includes A Novel Closed Loop Feedback Control System At The Antenna And From The Plasma. This Eliminates The Need For Lossy Transformers And Other Non-Ideal Components. The Rf Amplifier Will Be Prototyped In Phase I In Preparation For A Plasma Heating Experiment In Phase Ii.
- 7 Jun 2018
- Igf::Ot::Igf High Power Nuclear Fusion Propulsion Systems Will Require High Efficiency Radio-Frequency Heating Systems In The Mhz Range For Plasma Heating. This Proposal Is For A Novel Scalable Solid State Class E Amplifier Using Silicon Carbide Switching Transistors For Plasma Heating. This System Is Potentially 100% Efficient Compared To 40% For Linear Amplifiers And Can Be Scaled To Any Desired Size By Adding Additional Segments In Parallel. The System Includes A Novel Closed Loop Feedback Control System At The Antenna And From The Plasma. This Eliminates The Need For Lossy Transformers And Other Non-Ideal Components. The Rf Amplifier Will Be Prototyped In Phase I In Preparation For A Plasma Heating Experiment In Phase Ii.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,869.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0218
- This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies.
- 23 Apr 2020
- This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,981.00
- National Aeronautics And Space Administration (Nasa)
- NNX17CC74P
- Igf::Ot::Igf This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies. Our Goal Will Be To Design Space Coils Using The Latest High Temperature Superconductors. The Coils Will Be Operated At Medium Temperature, Between 20 And 30 K, Which Eases The Cooling Requirements And Temperature Margins Compared To 4K Low-Temperature Conductors. This Also Increases The Critical Currents Providing More Margin For Neutron Radiation Damage, Possibly Reducing Shielding. The Coils Will Have Highly Efficient Cooling Systems, Be Low Mass And Require Minimum Structural Mass. Bath Cooling And Conduit Cooling Will Be Compared. There Is Likely An Optimum Operating Temperature Which Minimizes The Mass Of Both The Conductors, Shielding, And Cooling Systems. Given The Rapid Advancement Of Hts Materials Determining The Feasibility Of Such An Optimal Coil Design Requires Detailed Research Into The State-Of-The-Art. Our Partner, Pppl, Will Provide Expertise On Coil Specifications And Magnet Design. Pppl Is The Only Institution In The World Where Active Research On The Physics And Technology Of Small, Steady-State Fusion Devices Is Being Performed. Pss Will Manage The Design Process And Study Closed Loop Cooling Issues. We Will Design A Phase Ii Experiment To Build One Or More 2 Tesla Coils And Potentially Integrate Them Into The Existing Plasma Experiment At Pppl. Our Example Mission Will Be A Neptune Orbiter Which Is On The Nasa Roadmap As A High Priority Mission And Present A Challenging On-Orbit Radiation Environment.
- 8 Jun 2018
- Igf::Ot::Igf This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies. Our Goal Will Be To Design Space Coils Using The Latest High Temperature Superconductors. The Coils Will Be Operated At Medium Temperature, Between 20 And 30 K, Which Eases The Cooling Requirements And Temperature Margins Compared To 4K Low-Temperature Conductors. This Also Increases The Critical Currents Providing More Margin For Neutron Radiation Damage, Possibly Reducing Shielding. The Coils Will Have Highly Efficient Cooling Systems, Be Low Mass And Require Minimum Structural Mass. Bath Cooling And Conduit Cooling Will Be Compared. There Is Likely An Optimum Operating Temperature Which Minimizes The Mass Of Both The Conductors, Shielding, And Cooling Systems. Given The Rapid Advancement Of Hts Materials Determining The Feasibility Of Such An Optimal Coil Design Requires Detailed Research Into The State-Of-The-Art. Our Partner, Pppl, Will Provide Expertise On Coil Specifications And Magnet Design. Pppl Is The Only Institution In The World Where Active Research On The Physics And Technology Of Small, Steady-State Fusion Devices Is Being Performed. Pss Will Manage The Design Process And Study Closed Loop Cooling Issues. We Will Design A Phase Ii Experiment To Build One Or More 2 Tesla Coils And Potentially Integrate Them Into The Existing Plasma Experiment At Pppl. Our Example Mission Will Be A Neptune Orbiter Which Is On The Nasa Roadmap As A High Priority Mission And Present A Challenging On-Orbit Radiation Environment.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,973.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0218
- This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies. Our Strategy For Pfrc Has Evolved Since Our Phase I Proposal, And We Now Propose A Hybrid Magnet Approach: A Combination Of So-Called Dry Conduction-Cooled Low-Temperature (Lts) Superconductor Magnets And High-Temperature (Hts) Magnets That Are Operated At Low Temperature For Maximum Current At High Fields. Conduction-Cooled Lts Magnets Are Becoming State-Of-The-Art For Mri Machines, And Reduce Coolant Requirements From 1000 S Of Liters Of Helium Over The Lifetime Of The Machine To A Few Liters In A Closed Cryocooler. This Is With A Mass Penalty For Cooling Of Only About 5%. These Lowcoolant Lts Magnets, Producing A Field Of 5 To 6 T, Will Have Excellent Safety Margin In Both Critical Current And Field And Will Have A Clear Path To Space Applications. Pfrc Also Requires Higher-Field Nozzle Magnets Producing Fields Of 20 To 30 T. These Would Utilize Hts Superconductors Operated At Low Temperatures Of About 10 K. All Coils Will Require Highly Efficient Cooling Systems, Excellent Mechanical Support, And Overall Low Mass Including Structural Components. Our Partner, Pppl, Is The Only Institution In The World Where Active Research On The Physics And Technology Of Small, Steady-State Fusion Devices Is Being Performed. We Propose A Phase Ii Experiment To Build A 0.5 Tesla Lts Magnet With A Split Pair Of Winding Packs, To Mimic A Subset Of The Pfrc Magnets. A Separate Pulsed Copper Test Coil To Simulation The Plasma Will Be Used To Study The Effects On The Magnet Of Frc Formation, Which Will Occur In A Fraction Of A Second And Result In Large Increases In Magnetic Field At The Windings. In Parallel, We Will Continue To Advance The Design Of The Hts Nozzle Magnets, Seeking The Lowest Mass Solution.
- 20 Sep 2018
- This Proposal Focuses On The Superconducting Coils Subsystem, A Critical Subsystem For The Pfrc Reactor And Direct Fusion Drive And Other Fusion And Electric Propulsion Technologies. Our Strategy For Pfrc Has Evolved Since Our Phase I Proposal, And We Now Propose A Hybrid Magnet Approach: A Combination Of So-Called Dry Conduction-Cooled Low-Temperature (Lts) Superconductor Magnets And High-Temperature (Hts) Magnets That Are Operated At Low Temperature For Maximum Current At High Fields. Conduction-Cooled Lts Magnets Are Becoming State-Of-The-Art For Mri Machines, And Reduce Coolant Requirements From 1000 S Of Liters Of Helium Over The Lifetime Of The Machine To A Few Liters In A Closed Cryocooler. This Is With A Mass Penalty For Cooling Of Only About 5%. These Lowcoolant Lts Magnets, Producing A Field Of 5 To 6 T, Will Have Excellent Safety Margin In Both Critical Current And Field And Will Have A Clear Path To Space Applications. Pfrc Also Requires Higher-Field Nozzle Magnets Producing Fields Of 20 To 30 T. These Would Utilize Hts Superconductors Operated At Low Temperatures Of About 10 K. All Coils Will Require Highly Efficient Cooling Systems, Excellent Mechanical Support, And Overall Low Mass Including Structural Components. Our Partner, Pppl, Is The Only Institution In The World Where Active Research On The Physics And Technology Of Small, Steady-State Fusion Devices Is Being Performed. We Propose A Phase Ii Experiment To Build A 0.5 Tesla Lts Magnet With A Split Pair Of Winding Packs, To Mimic A Subset Of The Pfrc Magnets. A Separate Pulsed Copper Test Coil To Simulation The Plasma Will Be Used To Study The Effects On The Magnet Of Frc Formation, Which Will Occur In A Fraction Of A Second And Result In Large Increases In Magnetic Field At The Windings. In Parallel, We Will Continue To Advance The Design Of The Hts Nozzle Magnets, Seeking The Lowest Mass Solution.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,981.00
- National Aeronautics And Space Administration (Nasa)