Transition45 Technologies Inc

CAGE Code: 444C9

NCAGE Code: 444C9

Status: Active

Type: Commercial Supplier

Dun & Bradstreet (DUNS): 621604128

Summary

Transition45 Technologies Inc is an Active Commercial Supplier with the Cage Code 444C9 and is tracked by Dun & Bradstreet under DUNS Number 621604128..

Address

1739 N Case St
Orange CA 92865-4211
United States

Points of Contact

No Points of Contact...

Related Information

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CAGE Code FAQ Frequently Asked Questions (FAQ) for CAGE 444C9

What is CAGE Code 444C9?
444C9 is the unique identifier used by NATO Organizations to reference the physical entity known as Transition45 Technologies Inc located at 1739 N Case St, Orange CA 92865-4211, United States.
Who is CAGE Code 444C9?
444C9 refers to Transition45 Technologies Inc located at 1739 N Case St, Orange CA 92865-4211, United States.
Where is CAGE Code 444C9 Located?
CAGE Code 444C9 is located in Orange, CA, USA.

Contracting History for CAGE 444C9 Contracting History for CAGE 444C9 Most Recent 25 Records

80NSSC19C0201
This Sbir Phase Ii Effort Will Continue To Develop And Then Scale Up A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten.
13 Aug 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$750,000.00
80NSSC19C0201
This Sbir Phase Ii Effort Will Continue To Develop And Then Scale Up A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten.
18 Sep 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$750,000.00
80NSSC19C0201
This Sbir Phase Ii Effort Will Continue To Develop And Then Scale Up A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten.
25 Aug 2020
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$750,000.00
80NSSC19C0201
Eo14042 This Sbir Phase Ii Effort Will Continue To Develop And Then Scale Up A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten.
16 Feb 2023
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$189,213.00
80NSSC19C0201
This Sbir Phase Ii Effort Will Continue To Develop And Then Scale Up A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten.
10 Nov 2020
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$750,000.00
80NSSC19C0201
Eo14042 This Sbir Phase Ii Effort Will Continue To Develop And Then Scale Up A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten.
14 Oct 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$750,000.00
SP470122P0029
Sbir Phase I Award Sp470122p0029 Nce Mod P00001
25 Apr 2022
Dcso Philadelphia
Department Of Defense (Dod)
$200,000.00
80NSSC20C0352
More Durable Pin Tools For Friction Stir Welding
24 Aug 2020
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$124,999.00
80NSSC18P2172
This Sbir Phase I Effort Will Develop And Demonstrate A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten. Tungsten, With Its Many Unique Characteristics, Plays An Important Role In Nuclear Reactors Including For The Nuclear Thermal Propulsion Engine. The Refractory Metal, However, Still Has A Number Of Shortcomings Which Still Need To Be Addressed. These Include A High Ductile-To-Brittle Transition Temperature, Low Ductility And Poor Fracture Toughness, Low Machinability And Fabricability, Low-Temperature Brittleness, Radiation-Induced Brittleness, And A Relatively Low Recrystallization (Rx) Temperature Compared To Its Operation Temperature. The Use Of W Above Its Rx Temperature Interminably Can Be Unsafe Because Its Mechanical Properties Decrease In Such An Environment. Low-Temperature Brittleness Also Imposes Restrictions On The Application Of W As A Structural Material. And, Given Its High Hardness, High Brittleness, And Poor Machinability, W Parts Can Be Very Costly And Time-Consuming To Manufacture. Past Efforts To Increase The Ductility Of W Were Primarily Directed On Alloying, Grain Refinement, Extreme Working, Area Reductions, Impurity Reductions, And Heat Treatments. While Ductile W Currently Exists In Wire Form (E.G., Filaments) Through Extensive Working And Area Reduction, This Approach Is Clearly Not Practical For Applications Where Bulk Size Parts Are Needed.
12 Feb 2019
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$125,000.00
80NSSC20C0352
Eo14042 More Durable Pin Tools For Friction Stir Welding
10 Nov 2022
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$124,999.00
80NSSC20C0352
More Durable Pin Tools For Friction Stir Welding
9 Sep 2021
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$124,999.00
80NSSC18P2172
This Sbir Phase I Effort Will Develop And Demonstrate A Novel Manufacturing Process Based On Severe Plastic Deformation (Spd) To Refine And Enhance The Microstructure-Properties Of Bulk Tungsten. Tungsten, With Its Many Unique Characteristics, Plays An Important Role In Nuclear Reactors Including For The Nuclear Thermal Propulsion Engine. The Refractory Metal, However, Still Has A Number Of Shortcomings Which Still Need To Be Addressed. These Include A High Ductile-To-Brittle Transition Temperature, Low Ductility And Poor Fracture Toughness, Low Machinability And Fabricability, Low-Temperature Brittleness, Radiation-Induced Brittleness, And A Relatively Low Recrystallization (Rx) Temperature Compared To Its Operation Temperature. The Use Of W Above Its Rx Temperature Interminably Can Be Unsafe Because Its Mechanical Properties Decrease In Such An Environment. Low-Temperature Brittleness Also Imposes Restrictions On The Application Of W As A Structural Material. And, Given Its High Hardness, High Brittleness, And Poor Machinability, W Parts Can Be Very Costly And Time-Consuming To Manufacture. Past Efforts To Increase The Ductility Of W Were Primarily Directed On Alloying, Grain Refinement, Extreme Working, Area Reductions, Impurity Reductions, And Heat Treatments. While Ductile W Currently Exists In Wire Form (E.G., Filaments) Through Extensive Working And Area Reduction, This Approach Is Clearly Not Practical For Applications Where Bulk Size Parts Are Needed.
26 Jul 2018
Nasa Shared Services Center
National Aeronautics And Space Administration (Nasa)
$125,000.00