Alliant Techsystems Operations Llc
CAGE Code: 06426
NCAGE Code: 06426
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 788102833
Summary
Alliant Techsystems Operations Llc is an Active Commercial Supplier with the Cage Code 06426 and is tracked by Dun & Bradstreet under DUNS Number 788102833..
Address
77 Raynor Ave
Ronkonkoma NY 11779-6649
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 06426
- What is CAGE Code 06426?
- 06426 is the unique identifier used by NATO Organizations to reference the physical entity known as Alliant Techsystems Operations Llc located at 77 Raynor Ave, Ronkonkoma NY 11779-6649, United States.
- Who is CAGE Code 06426?
- 06426 refers to Alliant Techsystems Operations Llc located at 77 Raynor Ave, Ronkonkoma NY 11779-6649, United States.
- Where is CAGE Code 06426 Located?
- CAGE Code 06426 is located in Ronkonkoma, NY, USA.
- How Many NSNs Does CAGE Code 06426 Supply?
- CAGE Code 06426 has been assigned as an approved source for 8 NSNs (National Stock Numbers and NATO Stock Numbers).
Contracting History for CAGE 06426 Most Recent 25 Records
- NNC12TA71T
- Propellant Testing For Mars Ascent Vehicle The Tasks Involved In This Effort Include: 1. The Contractor Shall Perform Propellant Development And Characterization Testing To Demonstrate The Feasibility Of The Proposed Propellant Formulation To Meet The Mav Requirements.
- 16 Apr 2015
- Propellant Testing For Mars Ascent Vehicle The Tasks Involved In This Effort Include: 1. The Contractor Shall Perform Propellant Development And Characterization Testing To Demonstrate The Feasibility Of The Proposed Propellant Formulation To Meet The Mav Requirements.
- Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $558,776.81
- National Aeronautics And Space Administration (Nasa)
- NNL06AA91T
- Fabrication Of New Mach 5 Nozzle For The Eight Foo T High Temperature Tunnel
- 18 Sep 2013
- Fabrication Of New Mach 5 Nozzle For The Eight Foo T High Temperature Tunnel
- Langley Research Center
- National Aeronautics And Space Administration (Nasa)
- $2,239,020.00
- National Aeronautics And Space Administration (Nasa)
- NNC13TB07T
- Nasa Has Identified The Need For Risk Reduction With Respect To The First Stage Of A Two Stage Mav, Which Will Be Capable Of Injecting An Orbiting Sample Into Mars Orbit. The First Stage Has Been Chosen Because Many Challenges Lie In Its Design. Both Stages Are Assumed To Be Solid Rocket Motors With A Propellant Capable Of Low Temperature Storage And Operation. The First Stage Is The Larger Of The Two Motors, Making Grain Stresses More Pronounced. It Also Utilized Thrust Vector Control (Tvc), Requiring S Tvc System To Be Adapted For This Application. The Second Stage Guidance Is Still Being Traded Between Spinning And Tvc. There Is A Strong Desire To Use Low Cost, High Heritage Components Where Possible. The Mav Must Survive Earth Launch, Cruise Transit, Entry Descent And Landing As Well As Mars Surface Environments. See The Attached Environmental Requirements Document (Erd) For Detailed Environmental Specifications. General: The Strawman Mav Design Assumes That It Will Be Lowered To The Surface Of Mars On A Heritage, Sky-Crane Lander. Propellant Mass Is Based On A Metastudy Of ~20 Years Of Solid Propellant Mav Designs. The Current Maximum Outer Diameter (Not Including Rcs Or Connection Adapters) Is Assumed To Be 15 Inches And The Maximum Stage 1 Motor Length Is 0.9M. Reductions In Envelope Are Desirable As These Are Preliminary Estimates Of The Geometry. All Masses Have Assumed A Current Best Estimate Plus 43% Margin. While This Contingency May Seem High For A Solid Rocket Motor, It Is Expected That The System Design Will Require Any Additional Margin Provided By The Propulsion System. It Is Assumed That Any Residual Margin Will Be Compensated For By Offloading Propellant (≪20%) Or Adding Ballast.
- 3 Jun 2014
- Nasa Has Identified The Need For Risk Reduction With Respect To The First Stage Of A Two Stage Mav, Which Will Be Capable Of Injecting An Orbiting Sample Into Mars Orbit. The First Stage Has Been Chosen Because Many Challenges Lie In Its Design. Both Stages Are Assumed To Be Solid Rocket Motors With A Propellant Capable Of Low Temperature Storage And Operation. The First Stage Is The Larger Of The Two Motors, Making Grain Stresses More Pronounced. It Also Utilized Thrust Vector Control (Tvc), Requiring S Tvc System To Be Adapted For This Application. The Second Stage Guidance Is Still Being Traded Between Spinning And Tvc. There Is A Strong Desire To Use Low Cost, High Heritage Components Where Possible. The Mav Must Survive Earth Launch, Cruise Transit, Entry Descent And Landing As Well As Mars Surface Environments. See The Attached Environmental Requirements Document (Erd) For Detailed Environmental Specifications. General: The Strawman Mav Design Assumes That It Will Be Lowered To The Surface Of Mars On A Heritage, Sky-Crane Lander. Propellant Mass Is Based On A Metastudy Of ~20 Years Of Solid Propellant Mav Designs. The Current Maximum Outer Diameter (Not Including Rcs Or Connection Adapters) Is Assumed To Be 15 Inches And The Maximum Stage 1 Motor Length Is 0.9M. Reductions In Envelope Are Desirable As These Are Preliminary Estimates Of The Geometry. All Masses Have Assumed A Current Best Estimate Plus 43% Margin. While This Contingency May Seem High For A Solid Rocket Motor, It Is Expected That The System Design Will Require Any Additional Margin Provided By The Propulsion System. It Is Assumed That Any Residual Margin Will Be Compensated For By Offloading Propellant (≪20%) Or Adding Ballast.
- Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $701,399.00
- National Aeronautics And Space Administration (Nasa)
- NNL07AE42T
- Nnl07ae42t New Task For The 8Ft Htt New Mach 3 Nozzle - Design, Fabrication And Assembly Of The New Nozzle And Install In The Nasa Larc 8Ft High Temperature Tunnel
- 9 Sep 2014
- Nnl07ae42t New Task For The 8Ft Htt New Mach 3 Nozzle - Design, Fabrication And Assembly Of The New Nozzle And Install In The Nasa Larc 8Ft High Temperature Tunnel
- Langley Research Center
- National Aeronautics And Space Administration (Nasa)
- $1,948,889.72
- National Aeronautics And Space Administration (Nasa)
- NNL08AD46T
- Nasa Langley Research Center Will Be Participating In Up Coming Projects That Will Require The 8-Ft High Temperature Tunnel To Test Large Scale Propulsion Ground Test Articles And Flight Vehicles. In Preparation For These Projects The Facility Needs To Determine The Feasibility Of Accommodating Large Scale Test Articles, Integration And Facility Operations/Interactions, At Conditions That Are Currently Out Of The Facilities Capabilities. The Objectives Of This Task Order Are To Resolve Ground Testing Issues Related To These Large Scale Test Articles Using A Blockage Model And Develop Test Capabilities Required To Meet Program Requirements. In Order To Achieve The Test Capabilities The Facility Will Require A New Mach 4 And Mach 6 Nozzle. These New Nozzles Will Be An Interagral Part Of The 8-Ft Htt At Nasa Langley Research Center. The New Nozzles Will Provide The Existing Facility Expanded Capability Required To Meet The Testing Goals Of Test Programs Present And Future. Large Scale Test Articles Pose Issues With Accurately Determining Blockage Effects Due To Their Complex Shapes And The Resulting Complex Flow Interactions Between The Large Scale Test Article And The Facility. A Blockage Model Will Help Resolve Most Of These Issues In Preparation For Ground Testing Large Scale Test Articles. The Purpose Of This Task Order Is To Obtain The Designs, Analysis, Manufacturing Schedules And Estimates Of Long Lead Items For A New Mach 4 And New Mach 6 Nozzles As Well A Trade Study For A Large Scale Blockage Model. This Task Order Is Broken Up Into 3 Main Sections: Mach 4 Nozzle (Design&Analysis), Mach 6 Nozzle (Design&Analysis) And A Blockage Model (Trade Study). Each Have Specific Requirements And Have Specific Due Dates.
- 9 Sep 2014
- Nasa Langley Research Center Will Be Participating In Up Coming Projects That Will Require The 8-Ft High Temperature Tunnel To Test Large Scale Propulsion Ground Test Articles And Flight Vehicles. In Preparation For These Projects The Facility Needs To Determine The Feasibility Of Accommodating Large Scale Test Articles, Integration And Facility Operations/Interactions, At Conditions That Are Currently Out Of The Facilities Capabilities. The Objectives Of This Task Order Are To Resolve Ground Testing Issues Related To These Large Scale Test Articles Using A Blockage Model And Develop Test Capabilities Required To Meet Program Requirements. In Order To Achieve The Test Capabilities The Facility Will Require A New Mach 4 And Mach 6 Nozzle. These New Nozzles Will Be An Interagral Part Of The 8-Ft Htt At Nasa Langley Research Center. The New Nozzles Will Provide The Existing Facility Expanded Capability Required To Meet The Testing Goals Of Test Programs Present And Future. Large Scale Test Articles Pose Issues With Accurately Determining Blockage Effects Due To Their Complex Shapes And The Resulting Complex Flow Interactions Between The Large Scale Test Article And The Facility. A Blockage Model Will Help Resolve Most Of These Issues In Preparation For Ground Testing Large Scale Test Articles. The Purpose Of This Task Order Is To Obtain The Designs, Analysis, Manufacturing Schedules And Estimates Of Long Lead Items For A New Mach 4 And New Mach 6 Nozzles As Well A Trade Study For A Large Scale Blockage Model. This Task Order Is Broken Up Into 3 Main Sections: Mach 4 Nozzle (Design&Analysis), Mach 6 Nozzle (Design&Analysis) And A Blockage Model (Trade Study). Each Have Specific Requirements And Have Specific Due Dates.
- Langley Research Center
- National Aeronautics And Space Administration (Nasa)
- $377,993.00
- National Aeronautics And Space Administration (Nasa)
Supply Items Approved for CAGE 06426 Page 1 of 1
- 2612522-1
- RNCC: 3 | RNVC: 2 | DAC: 4
- 2605886-1
- RNCC: 5 | RNVC: 1 | DAC: 5
- PSG1
- RNCC: 3 | RNVC: 2 | DAC: 4
- 0524-80
- RNCC: 5 | RNVC: 9 | DAC: 5
- 5363-87-701-1
- RNCC: 3 | RNVC: 2 | DAC: 5
- B8410-01-750
- RNCC: 3 | RNVC: 2 | DAC: 2
- 465-0868
- RNCC: 5 | RNVC: 1 | DAC: 3
- 465-4407
- RNCC: 3 | RNVC: 2 | DAC: D