Little Prairie Services Llc
CAGE Code: 4L3R2
NCAGE Code: 4L3R2
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 170301639
Summary
Little Prairie Services Llc is an Active Commercial Supplier with the Cage Code 4L3R2 and is tracked by Dun & Bradstreet under DUNS Number 170301639..
Address
14 Dunkin Rd
Edgewood NM 87015-9798
United States
Points of Contact
- Telephone:
- 5052208029
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Frequently Asked Questions (FAQ) for CAGE 4L3R2
- What is CAGE Code 4L3R2?
- 4L3R2 is the unique identifier used by NATO Organizations to reference the physical entity known as Little Prairie Services Llc located at 14 Dunkin Rd, Edgewood NM 87015-9798, United States.
- Who is CAGE Code 4L3R2?
- 4L3R2 refers to Little Prairie Services Llc located at 14 Dunkin Rd, Edgewood NM 87015-9798, United States.
- Where is CAGE Code 4L3R2 Located?
- CAGE Code 4L3R2 is located in Edgewood, NM, USA.
Contracting History for CAGE 4L3R2 Most Recent 25 Records
- 80NSSC22CA017
- E014042 Sbir Phase Ntr Fuel Testing In Mit Reactor Facilities
- 13 Apr 2022
- E014042 Sbir Phase Ntr Fuel Testing In Mit Reactor Facilities
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,117,664.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC22CA017
- Sbir Phase Ntr Fuel Testing In Mit Reactor Facilities
- 24 Oct 2023
- Sbir Phase Ntr Fuel Testing In Mit Reactor Facilities
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,117,664.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC22CA017
- Sbir Phase Ntr Fuel Testing In Mit Reactor Facilities
- 16 Aug 2023
- Sbir Phase Ntr Fuel Testing In Mit Reactor Facilities
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,117,664.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0637
- Ntr Fuel Testing In Mit Reactor Facilities
- 24 Aug 2020
- Ntr Fuel Testing In Mit Reactor Facilities
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,925.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0185
- Nuclear Thermal Propulsion (Ntp) Offers High Promise To Reduce Launch Mass, Decrease Mission Costs And Increase Mission Effectiveness, Particularly For Crewed Missions To The Planets. However, Ntp Has Been Plagued With High Uncertainties In Cost, Schedule And Safety, Particularly Launch Safety. To Reduce Programmatic Uncertainty, An Unambiguous Approach To Documenting Ntp Safety Prior To, During And After Launch Needs To Be Made. Until Recently, The Multi-Physics Models And Computing Power Were Not Available To Perform Compelling Analyses, And Testing Is Prohibitively Expensive, And Unrevealing In Many Cases. This Proposal Directly Addresses Programmatic Uncertainty By Providing Benchmarked, Definitive Product Capable Of Documenting The Safety Of A Ntp System During All Launch Phases. The Proposal Takes Work Performed By The Sbc Under Ir&D Which Has Performed Detailed Hydrocode Modeling Of A Ntp Impacting An Unyielding Surface From Heights Of 50 And 150 Meters. To Initiate The Effort, It Is Important To Start With Simple Compaction Model, Which Was Accomplished In Phase I With The Taylor Impact Simulation. Instead Of A Single Neutronics Code, Lps Demonstrated Viability With Three Codes To Better Insure Reliable Results. Phase Ii Will Extend This Work. It Will Continue To Update The Sccte-2 Ntr Design And Include Any Design Modifications By Nasa Contractors. The Ntr Model Will Be Updated To Include Important Peripherals Suchs As Turbooo Pump Assemblies, Thrust Vector Control Hardware, Plumbing And A Propellant Tank. These Are Essential Items For A More Realistic Impact Scenario. Further, During Phase I, Lps Determined There Are A Number Of Materials Whose Mechanical Database Is Insufficient For Unambiguous Hydrocode Simulations. Lps Will Deliver A Comprhensive Test Program Plan, Costs And Schedule To Resolve These Deficiencies. The Technical Readiness Will Be Improved So End To End Software Elements Are Implemented And Interfaced With Existing System Concepts.
- 23 Jun 2021
- Nuclear Thermal Propulsion (Ntp) Offers High Promise To Reduce Launch Mass, Decrease Mission Costs And Increase Mission Effectiveness, Particularly For Crewed Missions To The Planets. However, Ntp Has Been Plagued With High Uncertainties In Cost, Schedule And Safety, Particularly Launch Safety. To Reduce Programmatic Uncertainty, An Unambiguous Approach To Documenting Ntp Safety Prior To, During And After Launch Needs To Be Made. Until Recently, The Multi-Physics Models And Computing Power Were Not Available To Perform Compelling Analyses, And Testing Is Prohibitively Expensive, And Unrevealing In Many Cases. This Proposal Directly Addresses Programmatic Uncertainty By Providing Benchmarked, Definitive Product Capable Of Documenting The Safety Of A Ntp System During All Launch Phases. The Proposal Takes Work Performed By The Sbc Under Ir&D Which Has Performed Detailed Hydrocode Modeling Of A Ntp Impacting An Unyielding Surface From Heights Of 50 And 150 Meters. To Initiate The Effort, It Is Important To Start With Simple Compaction Model, Which Was Accomplished In Phase I With The Taylor Impact Simulation. Instead Of A Single Neutronics Code, Lps Demonstrated Viability With Three Codes To Better Insure Reliable Results. Phase Ii Will Extend This Work. It Will Continue To Update The Sccte-2 Ntr Design And Include Any Design Modifications By Nasa Contractors. The Ntr Model Will Be Updated To Include Important Peripherals Suchs As Turbooo Pump Assemblies, Thrust Vector Control Hardware, Plumbing And A Propellant Tank. These Are Essential Items For A More Realistic Impact Scenario. Further, During Phase I, Lps Determined There Are A Number Of Materials Whose Mechanical Database Is Insufficient For Unambiguous Hydrocode Simulations. Lps Will Deliver A Comprhensive Test Program Plan, Costs And Schedule To Resolve These Deficiencies. The Technical Readiness Will Be Improved So End To End Software Elements Are Implemented And Interfaced With Existing System Concepts.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,750.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0185
- Eo14042 Nuclear Thermal Propulsion (Ntp) Offers High Promise To Reduce Launch Mass, Decrease Mission Costs And Increase Mission Effectiveness, Particularly For Crewed Missions To The Planets. However, Ntp Has Been Plagued With High Uncertainties In Cost, Schedule And Safety, Particularly Launch Safety. To Reduce Programmatic Uncertainty, An Unambiguous Approach To Documenting Ntp Safety Prior To, During And After Launch Needs To Be Made. Until Recently, The Multi-Physics Models And Computing Power Were Not Available To Perform Compelling Analyses, And Testing Is Prohibitively Expensive, And Unrevealing In Many Cases. This Proposal Directly Addresses Programmatic Uncertainty By Providing Benchmarked, Definitive Product Capable Of Documenting The Safety Of A Ntp System During All Launch Phases. The Proposal Takes Work Performed By The Sbc Under Ir&D Which Has Performed Detailed Hydrocode Modeling Of A Ntp Impacting An Unyielding Surface From Heights Of 50 And 150 Meters. To Initiate The Effort, It Is Important To Start With Simple Compaction Model, Which Was Accomplished In Phase I With The Taylor Impact Simulation. Instead Of A Single Neutronics Code, Lps Demonstrated Viability With Three Codes To Better Insure Reliable Results. Phase Ii Will Extend This Work. It Will Continue To Update The Sccte-2 Ntr Design And Include Any Design Modifications By Nasa Contractors. The Ntr Model Will Be Updated To Include Important Peripherals Suchs As Turbooo Pump Assemblies, Thrust Vector Control Hardware, Plumbing And A Propellant Tank. These Are Essential Items For A More Realistic Impact Scenario. Further, During Phase I, Lps Determined There Are A Number Of Materials Whose Mechanical Database Is Insufficient For Unambiguous Hydrocode Simulations. Lps Will Deliver A Comprhensive Test Program Plan, Costs And Schedule To Resolve These Deficiencies. The Technical Readiness Will Be Improved So End To End Software Elements Are Implemented And Interfaced With Existing System Concepts.
- 24 Jan 2022
- Eo14042 Nuclear Thermal Propulsion (Ntp) Offers High Promise To Reduce Launch Mass, Decrease Mission Costs And Increase Mission Effectiveness, Particularly For Crewed Missions To The Planets. However, Ntp Has Been Plagued With High Uncertainties In Cost, Schedule And Safety, Particularly Launch Safety. To Reduce Programmatic Uncertainty, An Unambiguous Approach To Documenting Ntp Safety Prior To, During And After Launch Needs To Be Made. Until Recently, The Multi-Physics Models And Computing Power Were Not Available To Perform Compelling Analyses, And Testing Is Prohibitively Expensive, And Unrevealing In Many Cases. This Proposal Directly Addresses Programmatic Uncertainty By Providing Benchmarked, Definitive Product Capable Of Documenting The Safety Of A Ntp System During All Launch Phases. The Proposal Takes Work Performed By The Sbc Under Ir&D Which Has Performed Detailed Hydrocode Modeling Of A Ntp Impacting An Unyielding Surface From Heights Of 50 And 150 Meters. To Initiate The Effort, It Is Important To Start With Simple Compaction Model, Which Was Accomplished In Phase I With The Taylor Impact Simulation. Instead Of A Single Neutronics Code, Lps Demonstrated Viability With Three Codes To Better Insure Reliable Results. Phase Ii Will Extend This Work. It Will Continue To Update The Sccte-2 Ntr Design And Include Any Design Modifications By Nasa Contractors. The Ntr Model Will Be Updated To Include Important Peripherals Suchs As Turbooo Pump Assemblies, Thrust Vector Control Hardware, Plumbing And A Propellant Tank. These Are Essential Items For A More Realistic Impact Scenario. Further, During Phase I, Lps Determined There Are A Number Of Materials Whose Mechanical Database Is Insufficient For Unambiguous Hydrocode Simulations. Lps Will Deliver A Comprhensive Test Program Plan, Costs And Schedule To Resolve These Deficiencies. The Technical Readiness Will Be Improved So End To End Software Elements Are Implemented And Interfaced With Existing System Concepts.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,750.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0185
- Eo14042 Nuclear Thermal Propulsion (Ntp) Offers High Promise To Reduce Launch Mass, Decrease Mission Costs And Increase Mission Effectiveness, Particularly For Crewed Missions To The Planets. However, Ntp Has Been Plagued With High Uncertainties In Cost, Schedule And Safety, Particularly Launch Safety. To Reduce Programmatic Uncertainty, An Unambiguous Approach To Documenting Ntp Safety Prior To, During And After Launch Needs To Be Made. Until Recently, The Multi-Physics Models And Computing Power Were Not Available To Perform Compelling Analyses, And Testing Is Prohibitively Expensive, And Unrevealing In Many Cases. This Proposal Directly Addresses Programmatic Uncertainty By Providing Benchmarked, Definitive Product Capable Of Documenting The Safety Of A Ntp System During All Launch Phases. The Proposal Takes Work Performed By The Sbc Under Ir&D Which Has Performed Detailed Hydrocode Modeling Of A Ntp Impacting An Unyielding Surface From Heights Of 50 And 150 Meters. To Initiate The Effort, It Is Important To Start With Simple Compaction Model, Which Was Accomplished In Phase I With The Taylor Impact Simulation. Instead Of A Single Neutronics Code, Lps Demonstrated Viability With Three Codes To Better Insure Reliable Results. Phase Ii Will Extend This Work. It Will Continue To Update The Sccte-2 Ntr Design And Include Any Design Modifications By Nasa Contractors. The Ntr Model Will Be Updated To Include Important Peripherals Suchs As Turbooo Pump Assemblies, Thrust Vector Control Hardware, Plumbing And A Propellant Tank. These Are Essential Items For A More Realistic Impact Scenario. Further, During Phase I, Lps Determined There Are A Number Of Materials Whose Mechanical Database Is Insufficient For Unambiguous Hydrocode Simulations. Lps Will Deliver A Comprhensive Test Program Plan, Costs And Schedule To Resolve These Deficiencies. The Technical Readiness Will Be Improved So End To End Software Elements Are Implemented And Interfaced With Existing System Concepts.
- 12 Oct 2021
- Eo14042 Nuclear Thermal Propulsion (Ntp) Offers High Promise To Reduce Launch Mass, Decrease Mission Costs And Increase Mission Effectiveness, Particularly For Crewed Missions To The Planets. However, Ntp Has Been Plagued With High Uncertainties In Cost, Schedule And Safety, Particularly Launch Safety. To Reduce Programmatic Uncertainty, An Unambiguous Approach To Documenting Ntp Safety Prior To, During And After Launch Needs To Be Made. Until Recently, The Multi-Physics Models And Computing Power Were Not Available To Perform Compelling Analyses, And Testing Is Prohibitively Expensive, And Unrevealing In Many Cases. This Proposal Directly Addresses Programmatic Uncertainty By Providing Benchmarked, Definitive Product Capable Of Documenting The Safety Of A Ntp System During All Launch Phases. The Proposal Takes Work Performed By The Sbc Under Ir&D Which Has Performed Detailed Hydrocode Modeling Of A Ntp Impacting An Unyielding Surface From Heights Of 50 And 150 Meters. To Initiate The Effort, It Is Important To Start With Simple Compaction Model, Which Was Accomplished In Phase I With The Taylor Impact Simulation. Instead Of A Single Neutronics Code, Lps Demonstrated Viability With Three Codes To Better Insure Reliable Results. Phase Ii Will Extend This Work. It Will Continue To Update The Sccte-2 Ntr Design And Include Any Design Modifications By Nasa Contractors. The Ntr Model Will Be Updated To Include Important Peripherals Suchs As Turbooo Pump Assemblies, Thrust Vector Control Hardware, Plumbing And A Propellant Tank. These Are Essential Items For A More Realistic Impact Scenario. Further, During Phase I, Lps Determined There Are A Number Of Materials Whose Mechanical Database Is Insufficient For Unambiguous Hydrocode Simulations. Lps Will Deliver A Comprhensive Test Program Plan, Costs And Schedule To Resolve These Deficiencies. The Technical Readiness Will Be Improved So End To End Software Elements Are Implemented And Interfaced With Existing System Concepts.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,750.00
- National Aeronautics And Space Administration (Nasa)