Boulder Environmental Sciences And
Technology, Llc
Dba Boulder Environmental Sciences &
Technology Llc
CAGE Code: 4DML5
NCAGE Code: 4DML5
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 623842619
Summary
Boulder Environmental Sciences And, Technology, Llc, Dba Boulder Environmental Sciences &, Technology Llc is an Active Commercial Supplier with the Cage Code 4DML5 and is tracked by Dun & Bradstreet under DUNS Number 623842619..
Address
6201 Spine Rd Ste B
Boulder CO 80301-4114
United States
Points of Contact
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Frequently Asked Questions (FAQ) for CAGE 4DML5
- What is CAGE Code 4DML5?
- 4DML5 is the unique identifier used by NATO Organizations to reference the physical entity known as Boulder Environmental Sciences And Technology, Llc Dba Boulder Environmental Sciences & Technology Llc located at 6201 Spine Rd Ste B, Boulder CO 80301-4114, United States.
- Who is CAGE Code 4DML5?
- 4DML5 refers to Boulder Environmental Sciences And Technology, Llc Dba Boulder Environmental Sciences & Technology Llc located at 6201 Spine Rd Ste B, Boulder CO 80301-4114, United States.
- Where is CAGE Code 4DML5 Located?
- CAGE Code 4DML5 is located in Boulder, CO, USA.
Contracting History for CAGE 4DML5 Most Recent 25 Records
- 80NSSC22CA050
- Low-Loss Deployable Reflector Antenna At Frequencies Up To 200 Ghz For Small Satellites
- 18 May 2022
- Low-Loss Deployable Reflector Antenna At Frequencies Up To 200 Ghz For Small Satellites
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $799,978.00
- National Aeronautics And Space Administration (Nasa)
- FA945321P0512
- Hyperspectral Microwave Imaging Radiometer
- 7 Apr 2021
- Hyperspectral Microwave Imaging Radiometer
- Fa9453 Det 8 Afrl Pkv8
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 18 Dec 2020
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- Eo14042 The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 13 Oct 2021
- Eo14042 The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 5 Aug 2020
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- FA945321P0512
- Hyperspectral Microwave Imaging Radiometer
- 14 Jul 2021
- Hyperspectral Microwave Imaging Radiometer
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- 80NSSC21C0144
- Low-Loss Deployable Reflector Antenna At Frequencies Up To 200 Ghz For Small Satellites
- 3 May 2021
- Low-Loss Deployable Reflector Antenna At Frequencies Up To 200 Ghz For Small Satellites
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,994.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 29 Dec 2020
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0646
- Mesh-Based Reflector For Ka-Band Operation
- 30 Jun 2020
- Mesh-Based Reflector For Ka-Band Operation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $30,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0646
- Mesh-Based Reflector For Ka-Band Operation
- 9 Feb 2021
- Mesh-Based Reflector For Ka-Band Operation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $30,000.00
- National Aeronautics And Space Administration (Nasa)
- FA945321P0512
- Hyperspectral Microwave Imaging Radiometer
- 21 Jul 2021
- Hyperspectral Microwave Imaging Radiometer
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $150,000.00
- Department Of Defense (Dod)
- 80NSSC19C0646
- Mesh-Based Reflector For Ka-Band Operation
- 1 Dec 2020
- Mesh-Based Reflector For Ka-Band Operation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $30,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0646
- Mesh-Based Reflector For Ka-Band Operation
- 16 Sep 2020
- Mesh-Based Reflector For Ka-Band Operation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $30,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 23 May 2018
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $755,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 1 Apr 2020
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 24 Jun 2020
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- FA945319P0632
- Participation In An Air Force Sponsored Week Long Design Collaboration With Defense, International, And Commercial Stakeholders To Address The Feasibility Requirements For An Operational Demonstration.
- 31 May 2019
- Participation In An Air Force Sponsored Week Long Design Collaboration With Defense, International, And Commercial Stakeholders To Address The Feasibility Requirements For An Operational Demonstration.
- Fa9453 Afrl Rvk
- Department Of Defense (Dod)
- $74,997.00
- Department Of Defense (Dod)
- 80NSSC20P2351
- (1) 183Ghz Antenna System
- 28 Sep 2020
- (1) 183Ghz Antenna System
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $29,556.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0646
- Mesh-Based Reflector For Ka-Band Operation
- 25 Sep 2019
- Mesh-Based Reflector For Ka-Band Operation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $30,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0646
- Mesh-Based Reflector For Ka-Band Operation
- 23 Oct 2020
- Mesh-Based Reflector For Ka-Band Operation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $30,000.00
- National Aeronautics And Space Administration (Nasa)
- FA945319P0632
- Participation In An Air Force Sponsored Week Long Design Collaboration With Defense, International, And Commercial Stakeholders To Address The Feasibility Requirements For An Operational Demonstration.
- 28 Aug 2019
- Participation In An Air Force Sponsored Week Long Design Collaboration With Defense, International, And Commercial Stakeholders To Address The Feasibility Requirements For An Operational Demonstration.
- Dcma Western Regional Command
- Department Of Defense (Dod)
- $74,997.00
- Department Of Defense (Dod)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 7 Sep 2021
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0046
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- 26 Sep 2019
- The Goal Of This Project Is To Develop An Offset-Fed Paraboloidal Mesh Reflector Antenna For Operation Onboard Small, Low Cost Satellites Such As Cubesats, In The Frequency Range Up To 100 Ghz. The Phase Ii Component Of This Goal Is To Fully Test The Performance Characteristics Of A Prototype Deployable Antenna Reflector, With An Aperture Greater Than 0.5 M Under Controlled Conditions. The Mesh Used In The Reflector Is Gold Plated Molybdenum. The Weave Of The Mesh Will Be Developed Early In Phase Ii To Achieve The Tight Tolerances Required For Operation Up To 100 Ghz (W-Band). Characterization Measurements Of The Currently Available Mesh Have Been Completed And Will Be Used As A Baseline To Quantify Improvements Measured From The Newly Developed Mesh Samples. Analysis Of Surface Error Contributions From Faceting, Thermal Stresses, Manufacturing Tolerances, And Operational Forces Will Be Performed. Micro-Machining And Small-Scale Manufacturing Techniques Will Be Refined To Achieve An Overall Reflector Surface Accuracy Of Less Than 60 Micrometers (1/50 Of The Wavelength At 100 Ghz). The Fully Constructed Mesh Reflector Antenna With Feed Will Be Measured To Obtain The Full Gain Pattern Of The Antenna To Characterize The Antenna Performance And Determine The Overall Efficiency Of The Mesh Reflector. The Deployment Mechanism Will Also Be Tested And Refined To Ensure Repeatable Operation Of The Antenna. The Proposed Antenna Can Be Stowed Within Less Than 1.5 U Of A Cubesat. Doing So Can Significantly Lower The Cost Of Any Satellite System Requiring A High Gain Reflector Antenna, Including Radars, Scatterometers, Radiometers, And Deep Space Communication Links. Successful Completion Of The Phase Ii Goals Will Increase The Technical Readiness Of The Project From Trl 3, At The End Of Phase I, To Trl 6.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $785,000.00
- National Aeronautics And Space Administration (Nasa)