Atk Space Systems Llc

CAGE Code: 18229

NCAGE Code: 18229

Status: Active

Type: Commercial Supplier

Dun & Bradstreet (DUNS): 131288391

CAGE 18229 Atk Space Systems Llc
CAGE 18229 Atk Space Systems Llc

Summary

Atk Space Systems Llc is an Active Commercial Supplier with the Cage Code 18229 and is tracked by Dun & Bradstreet under DUNS Number 131288391..

Address

6033 Bandini Blvd
Commerce CA 90040-2968
United States

Points of Contact

Telephone:
7142406521
Atk Space Systems Llc http://www.psi-pci.com/

Related Information

DUNS Report

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CAGE Code FAQ Frequently Asked Questions (FAQ) for CAGE 18229

What is CAGE Code 18229?
18229 is the unique identifier used by NATO Organizations to reference the physical entity known as Atk Space Systems Llc located at 6033 Bandini Blvd, Commerce CA 90040-2968, United States.
Who is CAGE Code 18229?
18229 refers to Atk Space Systems Llc located at 6033 Bandini Blvd, Commerce CA 90040-2968, United States.
Where is CAGE Code 18229 Located?
CAGE Code 18229 is located in Commerce, CA, USA.

Contracting History for CAGE 18229 Contracting History for CAGE 18229 Most Recent 25 Records

80GSFC21C0054
Roman Space Telescope Project Propellant Tanks
29 Sep 2022
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC21C0054
Roman Space Telescope Project Propellant Tanks
28 Aug 2023
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC21C0054
Roman Space Telescope Project Propellant Tanks
1 Feb 2023
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC21C0054
Roman Space Telescope Project Propellant Tanks
20 Jul 2023
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC21C0054
Roman Space Telescope Project Propellant Tanks
2 Jun 2023
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC21C0054
Roman Space Telescope Project Propellant Tanks
1 May 2023
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC21C0054
Eo14042 Roman Space Telescope Propellant Tanks
19 Nov 2021
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$2,622,747.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing; All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
16 May 2019
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,441,974.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing; All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
9 Jul 2019
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,441,974.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
24 Nov 2020
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
26 Feb 2021
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
31 Jan 2020
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
28 Apr 2021
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing; All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
30 Oct 2018
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,441,974.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
17 Dec 2020
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
23 Apr 2020
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
28 Aug 2020
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
19 Dec 2019
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
26 Jun 2020
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,711,241.00
80GSFC19C0003
This Procurement Is For A Space Flight Propellant Tank For The Plankton, Aerosol, Cloud, Ocean Ecosystem (Pace) Spacecraft. This Contract Includes The Fabricating, Test, Inspect, And Deliver Of One (1) Diaphragm Propellant Tank, Utilize An Existing Propellant Tank Simulator To Perform Diaphragm And Slosh Testing, And Perform Propellant Tank Vibration Testing. The Contractor Will Also Provide Gsfc No-Cost Use Of Their Propellant Tank Simulator For Supporting Propellant Tank Close Out Welding. This Simulator Will Be Shipped To Gsfc Upon Completion Of Slosh Testing. Pace Is Comprised Of Three Instruments, An Ocean Color Instrument (Oci) And Two Polarimeters (Harp2 And Spexone). The Oci Is The Primary Instrument On The Observatory And Is Being Developed At Gsfc. The Oci Is A Hyper-Spectral Scanning (Hss) Radiometer Designed To Measure Spectral Radiances From The Ultraviolet To Shortwave Infrared (Swir) To Enable Advanced Ocean Color And Heritage Cloud And Aerosol Particle Science. The Polarimeters Are Secondary Instruments On The Pace Observatory, Developed Outside Of Gsfc. Both Polarimeters Are Multi-Band, Multi-Angle Polarimeters Planned To Measure Spectral Polarized And Unpolarized Radiances To Enable Advanced Cloud And Aerosol Particle Science, As Well As Improved Atmospheric Correction For Ocean Color Activities. The Pace Mission Requires An Integrated Propulsion System. The Pace Propulsion Subsystem Consists Of The Components Required To Contain, Control, Monitor, And Utilize Hydrazine Propellant To Accomplish Orbit Maneuvering And Momentum Management Requirements. The Propulsion Subsystem Includes A Propellant Tank, Propellant Filter, Pressure Transducers, Surge Suppression Devices, Latching Isolation Valves, Fill And Drain Valves, Thrusters, And Interconnecting Tubing. The Propulsion Subsystem Also Includes Electrical Hardware Connecting Components To Avionics And Test Connectors, As Well As Heaters, Thermostats, And Sensors On The Propellant Lines And Components. The System Is An All Welded System Using Stainless Steel Tubing All Welds Are Radiographically Inspected Prior To The System Proof Pressure Test And Checked For Leakage After The System Proof Pressure Test. The Propulsion Subsystem Is A Monopropellant Hydrazine System Using Unregulated (Blowdown) Gaseous Helium Pressurization
29 Nov 2019
Nasa Goddard Space Flight Center
National Aeronautics And Space Administration (Nasa)
$1,441,974.00