Air Squared, Llc
CAGE Code: 1VAK0
NCAGE Code: 1VAK0
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 824841027
Summary
Air Squared, Llc is an Active Commercial Supplier with the Cage Code 1VAK0 and is tracked by Dun & Bradstreet under DUNS Number 824841027..
Address
675 E 124Th Ave
Thornton CO 80241-2411
United States
Points of Contact
No Points of Contact...
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Frequently Asked Questions (FAQ) for CAGE 1VAK0
- What is CAGE Code 1VAK0?
- 1VAK0 is the unique identifier used by NATO Organizations to reference the physical entity known as Air Squared, Llc located at 675 E 124Th Ave, Thornton CO 80241-2411, United States.
- Who is CAGE Code 1VAK0?
- 1VAK0 refers to Air Squared, Llc located at 675 E 124Th Ave, Thornton CO 80241-2411, United States.
- Where is CAGE Code 1VAK0 Located?
- CAGE Code 1VAK0 is located in Thornton, CO, USA.
Contracting History for CAGE 1VAK0 Most Recent 25 Records
- 80NSSC23CA068
- E014042 Sbir Phase Ii Helium Transfer Scroll Pump System (Htsps)
- 22 May 2023
- E014042 Sbir Phase Ii Helium Transfer Scroll Pump System (Htsps)
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $849,658.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC23CA068
- E014042 Sbir Phase Ii Helium Transfer Scroll Pump System (Htsps)
- 30 Aug 2023
- E014042 Sbir Phase Ii Helium Transfer Scroll Pump System (Htsps)
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $849,658.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC22PA934
- E014042 Sbir Phase I Helium Transfer Scroll Pump System (Htsps)
- 20 Jul 2022
- E014042 Sbir Phase I Helium Transfer Scroll Pump System (Htsps)
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $149,856.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC22CA145
- E014042 Sbir Phase Ii Phase Ii Lunar Isru Contaminant Tolerant Scroll Vacuum Pump (Ctsvp)
- 4 May 2022
- E014042 Sbir Phase Ii Phase Ii Lunar Isru Contaminant Tolerant Scroll Vacuum Pump (Ctsvp)
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,916.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0123
- Spinning Scroll Boost Compressor
- 29 Jun 2020
- Spinning Scroll Boost Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0123
- Spinning Scroll Boost Compressor
- 11 Feb 2021
- Spinning Scroll Boost Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,996.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0123
- Eo14042 Spinning Scroll Boost Compressor
- 13 Oct 2021
- Eo14042 Spinning Scroll Boost Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,996.00
- National Aeronautics And Space Administration (Nasa)
- H9240519P0041
- Feasibility Study, Sbir Phase I, Topic Socom192- 002, Advanced Decompression Pump For Manned Submersibles With A Diver-Lock Chamber
- 29 Aug 2019
- Feasibility Study, Sbir Phase I, Topic Socom192- 002, Advanced Decompression Pump For Manned Submersibles With A Diver-Lock Chamber
- Hq Ussocom
- Department Of Defense (Dod)
- $149,423.76
- Department Of Defense (Dod)
- N6833519C0495
- Research And Development
- 27 Aug 2019
- Research And Development
- Navair Warfare Ctr Aircraft Div Lke
- Department Of Defense (Dod)
- $139,944.00
- Department Of Defense (Dod)
- N6833519C0495
- Progress Report
- 7 Jun 2019
- Progress Report
- Navair Warfare Ctr Aircraft Div
- Department Of Defense (Dod)
- $139,944.00
- Department Of Defense (Dod)
- 80NSSC20C0229
- Vapor Compression Refrigeration System For Cold Storage On Spacecraft
- 14 Jul 2020
- Vapor Compression Refrigeration System For Cold Storage On Spacecraft
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $88,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0184
- The Proposed Innovation Is The World's First Cryogenic Spinning Scroll Pump (Cssp) Capable Of Pumping Liquid Methane Or Oxygen At Flows Of 8-10 Lbm/S. The Primary Goal Is To Develop A Versatile Proof Of Concept Cssp, Capable Of Pumping Liquid Or Two-Phase Methane Or Oxygen At A Wide Range Of Speeds (I.E. 1,000-8,000 Rpm) And A Wide Range Of Differential Pressures While Maintaining High-Reliability And A Compact Size. The Pump Will Be Configurable, To Allow Multiple Pumps To Be Placed In Series For High-Pressure Multi-Stage Operation. During Phase I, Air Squared Successfully Designed, Fabricated And Tested A Prototype Cssp On Liquid Nitrogen. For Cryogenic Pumping, State Of The Art (Soa), Consists Of Two Vastly Different Technology Options. Centrifugal Turbopumps And Positive Displacement Pumps. Turbopumps Utilize An Impeller-Inducer Combination That Relies On High Impeller Speeds To Create A Differential Pressure. While The High-Speed Operation Makes Turbopumps Compact, It Also Limits Bearing Life, Differential Pressure, And They Can't Handle Two-Phase Flow. Positive Displacement Pumps Can Handle Larger Pressure Differentials And Don't Have Issues With Two-Phase Flow. However, They Can't Achieve Speeds Over 3,000 Rpm Without Bulky And High-Load Bearings Making Them Less Desirable For Aerospace Applications. The Cssp Offers The Best Of Both Options. As A Positive Displacement Pump, It Can Achieve High-Pressures With Minimal Reduction In Flow And Pump Saturated Liquids At Low Net-Positive Suction Heads. Due To The Spinning Motion Of The Pump, Various Centrifugal Loads Are Eliminated Allowing Speeds Over 8,000 Rpm Possible And Making The Design Compact And Lightweight. Additionally, The Spinning Motion Of The Scrolls Eliminates The Need For A Counterbalance Common In Orbiting Scroll Designs. This Further Reduces Weight By Eliminating Counterweights And Eases Bearing Loads. Air Squared Believes The Proposed Cssp Is A Perfect Fit In Support Of Methane In-Space Propulsion.
- 9 Jul 2018
- The Proposed Innovation Is The World's First Cryogenic Spinning Scroll Pump (Cssp) Capable Of Pumping Liquid Methane Or Oxygen At Flows Of 8-10 Lbm/S. The Primary Goal Is To Develop A Versatile Proof Of Concept Cssp, Capable Of Pumping Liquid Or Two-Phase Methane Or Oxygen At A Wide Range Of Speeds (I.E. 1,000-8,000 Rpm) And A Wide Range Of Differential Pressures While Maintaining High-Reliability And A Compact Size. The Pump Will Be Configurable, To Allow Multiple Pumps To Be Placed In Series For High-Pressure Multi-Stage Operation. During Phase I, Air Squared Successfully Designed, Fabricated And Tested A Prototype Cssp On Liquid Nitrogen. For Cryogenic Pumping, State Of The Art (Soa), Consists Of Two Vastly Different Technology Options. Centrifugal Turbopumps And Positive Displacement Pumps. Turbopumps Utilize An Impeller-Inducer Combination That Relies On High Impeller Speeds To Create A Differential Pressure. While The High-Speed Operation Makes Turbopumps Compact, It Also Limits Bearing Life, Differential Pressure, And They Can't Handle Two-Phase Flow. Positive Displacement Pumps Can Handle Larger Pressure Differentials And Don't Have Issues With Two-Phase Flow. However, They Can't Achieve Speeds Over 3,000 Rpm Without Bulky And High-Load Bearings Making Them Less Desirable For Aerospace Applications. The Cssp Offers The Best Of Both Options. As A Positive Displacement Pump, It Can Achieve High-Pressures With Minimal Reduction In Flow And Pump Saturated Liquids At Low Net-Positive Suction Heads. Due To The Spinning Motion Of The Pump, Various Centrifugal Loads Are Eliminated Allowing Speeds Over 8,000 Rpm Possible And Making The Design Compact And Lightweight. Additionally, The Spinning Motion Of The Scrolls Eliminates The Need For A Counterbalance Common In Orbiting Scroll Designs. This Further Reduces Weight By Eliminating Counterweights And Eases Bearing Loads. Air Squared Believes The Proposed Cssp Is A Perfect Fit In Support Of Methane In-Space Propulsion.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $750,093.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21P1977
- Development Unit For In-Space Pneumatic Helium Transfer Compressor
- 22 Jun 2022
- Development Unit For In-Space Pneumatic Helium Transfer Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $178,296.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0049
- Nasa Is Looking For Solutions For Its Long-Term Or Distance Food Storage And Transport Applications. Achieving High Thermal Efficiencies And Reliability While Maintaining Volumetric And Mass Efficiency Has Been The Key Challenge With These Kinds Of Refrigeration/Freezing Systems In A Microgravity Environment. Previous State Of The Art Refrigerator/Freezer Systems Such As The Iss Rfr, Use Thermoelectric Thermal Control With Very Low Overall System Cop Of Around 0.36 (In Freezer Mode). Alternatively, Terrestrial Cold Food Storage Systems Utilize Much More Efficient Vapor Compression Thermal Control Systems, Making The Systems Lighter And More Compact. Currently, These Systems Do Not Have Provisions To Fulfill The Load And Reliability Requirements Of Space Applications And Are Also Not Designed For Microgravity Operation. An Example Would Be Kelvinator Kccf220qw Chest Freezer. This Freezer Can Maintain Temperatures As Low As 26?C At Cops Of Around 2.2 To 2.4. Air Squared Is Proposing The Development Of A Zero-Gravity Vapor Compression Refrigerator (Zvcr). The Zvcr Is An Oil-Free, Scroll Driven, Vapor Compression Food Storage System That Is Thermally Efficient, Lightweight And Reliable. Similar To Conventional Systems, The Zvcr Will Include Four Major Components: Compressor, Condenser, Expansion Device And Evaporator. But, Instead Of A Heavy And Oil Lubricated Working Fluid Compressor, It Will Use An Advanced Oil-Free Orbiting Type Scroll Compressor And Expander Developed By Air Squared. Its Oil-Free Design Will Remove System S Operational Reliance On Gravity While Keeping The Design Compact&Lightweight At Higher Efficiencies. For Expansion Work Recovery, A Scroll Expander Based On The Same Technology As The Compressor Will Be Used To Further Improve The System S Performance. Custom Heat Exchangers Will Be Designed For Efficient Operation In Microgravity While Considering The Size, Weight And Reliability Requirements.
- 3 Jun 2020
- Nasa Is Looking For Solutions For Its Long-Term Or Distance Food Storage And Transport Applications. Achieving High Thermal Efficiencies And Reliability While Maintaining Volumetric And Mass Efficiency Has Been The Key Challenge With These Kinds Of Refrigeration/Freezing Systems In A Microgravity Environment. Previous State Of The Art Refrigerator/Freezer Systems Such As The Iss Rfr, Use Thermoelectric Thermal Control With Very Low Overall System Cop Of Around 0.36 (In Freezer Mode). Alternatively, Terrestrial Cold Food Storage Systems Utilize Much More Efficient Vapor Compression Thermal Control Systems, Making The Systems Lighter And More Compact. Currently, These Systems Do Not Have Provisions To Fulfill The Load And Reliability Requirements Of Space Applications And Are Also Not Designed For Microgravity Operation. An Example Would Be Kelvinator Kccf220qw Chest Freezer. This Freezer Can Maintain Temperatures As Low As 26?C At Cops Of Around 2.2 To 2.4. Air Squared Is Proposing The Development Of A Zero-Gravity Vapor Compression Refrigerator (Zvcr). The Zvcr Is An Oil-Free, Scroll Driven, Vapor Compression Food Storage System That Is Thermally Efficient, Lightweight And Reliable. Similar To Conventional Systems, The Zvcr Will Include Four Major Components: Compressor, Condenser, Expansion Device And Evaporator. But, Instead Of A Heavy And Oil Lubricated Working Fluid Compressor, It Will Use An Advanced Oil-Free Orbiting Type Scroll Compressor And Expander Developed By Air Squared. Its Oil-Free Design Will Remove System S Operational Reliance On Gravity While Keeping The Design Compact&Lightweight At Higher Efficiencies. For Expansion Work Recovery, A Scroll Expander Based On The Same Technology As The Compressor Will Be Used To Further Improve The System S Performance. Custom Heat Exchangers Will Be Designed For Efficient Operation In Microgravity While Considering The Size, Weight And Reliability Requirements.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $753,397.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0050
- The Proposed Innovation Supports Technologies For In Situ Resource Utilization (Isru) Processes By Collecting And Pressurizing Gasses From The Mars Atmosphere For Eventual Oxygen Production By Use Of Solid Oxide Electrolysis (Soxe).
- 30 Mar 2020
- The Proposed Innovation Supports Technologies For In Situ Resource Utilization (Isru) Processes By Collecting And Pressurizing Gasses From The Mars Atmosphere For Eventual Oxygen Production By Use Of Solid Oxide Electrolysis (Soxe).
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $753,136.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0049
- Nasa Is Looking For Solutions For Its Long-Term Or Distance Food Storage And Transport Applications. Achieving High Thermal Efficiencies And Reliability While Maintaining Volumetric And Mass Efficiency Has Been The Key Challenge With These Kinds Of Refrigeration/Freezing Systems In A Microgravity Environment. Previous State Of The Art Refrigerator/Freezer Systems Such As The Iss Rfr, Use Thermoelectric Thermal Control With Very Low Overall System Cop Of Around 0.36 (In Freezer Mode). Alternatively, Terrestrial Cold Food Storage Systems Utilize Much More Efficient Vapor Compression Thermal Control Systems, Making The Systems Lighter And More Compact. Currently, These Systems Do Not Have Provisions To Fulfill The Load And Reliability Requirements Of Space Applications And Are Also Not Designed For Microgravity Operation. An Example Would Be Kelvinator Kccf220qw Chest Freezer. This Freezer Can Maintain Temperatures As Low As 26?C At Cops Of Around 2.2 To 2.4. Air Squared Is Proposing The Development Of A Zero-Gravity Vapor Compression Refrigerator (Zvcr). The Zvcr Is An Oil-Free, Scroll Driven, Vapor Compression Food Storage System That Is Thermally Efficient, Lightweight And Reliable. Similar To Conventional Systems, The Zvcr Will Include Four Major Components: Compressor, Condenser, Expansion Device And Evaporator. But, Instead Of A Heavy And Oil Lubricated Working Fluid Compressor, It Will Use An Advanced Oil-Free Orbiting Type Scroll Compressor And Expander Developed By Air Squared. Its Oil-Free Design Will Remove System S Operational Reliance On Gravity While Keeping The Design Compact&Lightweight At Higher Efficiencies. For Expansion Work Recovery, A Scroll Expander Based On The Same Technology As The Compressor Will Be Used To Further Improve The System S Performance. Custom Heat Exchangers Will Be Designed For Efficient Operation In Microgravity While Considering The Size, Weight And Reliability Requirements.
- 17 Jul 2020
- Nasa Is Looking For Solutions For Its Long-Term Or Distance Food Storage And Transport Applications. Achieving High Thermal Efficiencies And Reliability While Maintaining Volumetric And Mass Efficiency Has Been The Key Challenge With These Kinds Of Refrigeration/Freezing Systems In A Microgravity Environment. Previous State Of The Art Refrigerator/Freezer Systems Such As The Iss Rfr, Use Thermoelectric Thermal Control With Very Low Overall System Cop Of Around 0.36 (In Freezer Mode). Alternatively, Terrestrial Cold Food Storage Systems Utilize Much More Efficient Vapor Compression Thermal Control Systems, Making The Systems Lighter And More Compact. Currently, These Systems Do Not Have Provisions To Fulfill The Load And Reliability Requirements Of Space Applications And Are Also Not Designed For Microgravity Operation. An Example Would Be Kelvinator Kccf220qw Chest Freezer. This Freezer Can Maintain Temperatures As Low As 26?C At Cops Of Around 2.2 To 2.4. Air Squared Is Proposing The Development Of A Zero-Gravity Vapor Compression Refrigerator (Zvcr). The Zvcr Is An Oil-Free, Scroll Driven, Vapor Compression Food Storage System That Is Thermally Efficient, Lightweight And Reliable. Similar To Conventional Systems, The Zvcr Will Include Four Major Components: Compressor, Condenser, Expansion Device And Evaporator. But, Instead Of A Heavy And Oil Lubricated Working Fluid Compressor, It Will Use An Advanced Oil-Free Orbiting Type Scroll Compressor And Expander Developed By Air Squared. Its Oil-Free Design Will Remove System S Operational Reliance On Gravity While Keeping The Design Compact&Lightweight At Higher Efficiencies. For Expansion Work Recovery, A Scroll Expander Based On The Same Technology As The Compressor Will Be Used To Further Improve The System S Performance. Custom Heat Exchangers Will Be Designed For Efficient Operation In Microgravity While Considering The Size, Weight And Reliability Requirements.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,024,397.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC20C0228
- Vapor Compression Refrigeration System For Cold Storage On Spacecraft
- 14 Jul 2020
- Vapor Compression Refrigeration System For Cold Storage On Spacecraft
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $100,000.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC19C0396
- Phase I Sbir For Spinning Scroll Boost Compressor
- 18 Aug 2019
- Phase I Sbir For Spinning Scroll Boost Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,152.00
- National Aeronautics And Space Administration (Nasa)
- NNX17CM14P
- Igf::Ot::Igf The Innovation Is An Efficient, Compact, Lightweight, Reliable, Electric-Driven, Cryogenic Spinning Scroll Pump (Cssp) Capable Of Pumping Liquid Methane Or Oxygen At Flows Of 8-10 Lbm/S. The Pump Will Satisfy Propulsion Feed System Needs Stated In Sbir Research Topic Z10.02: Methane In-Space Propulsion. The Primary Goal Is To Develop A Versatile Cssp, Capable Of Pumping Liquid Or Two-Phase Methane Or Oxygen At A Wide Range Of Speeds (I.E. 1,000-8,000 Rpm) And A Wide Range Of Differential Pressures While Maintaining High Reliability And A Compact Size. For Cryogenic Pumping, State Of The Art (Soa), Consists Of Two Vastly Different Technology Options. Centrifugal Turbopumps And Positive Displacement Pumps. Turbopumps Utilize An Impeller-Inducer Combination That Relies On High Impeller Speeds To Create A Differential Pressure. While The High-Speed Operation Makes Turbopumps More Compact, It Also Limits Bearing Life, Differential Pressure, And They Can't Handle Two-Phase Flow. Positive Displacement Pumps Can Handle Larger Pressure Differentials And Don't Have Issues With Two-Phase Flow. However, They Can't Achieve Speeds Over 3,000 Rpm Without Bulky And High-Load Bearings. This Typically Makes Positive Displacement Pumps Larger, And Consequently, Less Desirable For Aerospace Applications. The Cssp Offers The Best Of Both Options. As A Positive Displacement Pump, It Can Achieve High-Pressure With Minimal Reduction In Flow And Pump Saturated Liquids At Low Net-Positive Suction Heads. Due To The Spinning Motion Of The Pump Various Centrifugal Loads Are Eliminated, With Reduced Loading, Speeds Over 8,000 Rpm Are Possible, Making The Design Compact And Lightweight. Additionally, The Spinning Motion Of The Scrolls Eliminates The Need For A Counterbalance Common In Orbiting Scroll Designs. This Further Reduces Weight By Eliminating Counterweights And Eases Bearing Loads. Air Squared Believes The Proposed Cssp Is A Perfect Fit In Support Of Methane In-Space Propulsion.
- 9 Jun 2017
- Igf::Ot::Igf The Innovation Is An Efficient, Compact, Lightweight, Reliable, Electric-Driven, Cryogenic Spinning Scroll Pump (Cssp) Capable Of Pumping Liquid Methane Or Oxygen At Flows Of 8-10 Lbm/S. The Pump Will Satisfy Propulsion Feed System Needs Stated In Sbir Research Topic Z10.02: Methane In-Space Propulsion. The Primary Goal Is To Develop A Versatile Cssp, Capable Of Pumping Liquid Or Two-Phase Methane Or Oxygen At A Wide Range Of Speeds (I.E. 1,000-8,000 Rpm) And A Wide Range Of Differential Pressures While Maintaining High Reliability And A Compact Size. For Cryogenic Pumping, State Of The Art (Soa), Consists Of Two Vastly Different Technology Options. Centrifugal Turbopumps And Positive Displacement Pumps. Turbopumps Utilize An Impeller-Inducer Combination That Relies On High Impeller Speeds To Create A Differential Pressure. While The High-Speed Operation Makes Turbopumps More Compact, It Also Limits Bearing Life, Differential Pressure, And They Can't Handle Two-Phase Flow. Positive Displacement Pumps Can Handle Larger Pressure Differentials And Don't Have Issues With Two-Phase Flow. However, They Can't Achieve Speeds Over 3,000 Rpm Without Bulky And High-Load Bearings. This Typically Makes Positive Displacement Pumps Larger, And Consequently, Less Desirable For Aerospace Applications. The Cssp Offers The Best Of Both Options. As A Positive Displacement Pump, It Can Achieve High-Pressure With Minimal Reduction In Flow And Pump Saturated Liquids At Low Net-Positive Suction Heads. Due To The Spinning Motion Of The Pump Various Centrifugal Loads Are Eliminated, With Reduced Loading, Speeds Over 8,000 Rpm Are Possible, Making The Design Compact And Lightweight. Additionally, The Spinning Motion Of The Scrolls Eliminates The Need For A Counterbalance Common In Orbiting Scroll Designs. This Further Reduces Weight By Eliminating Counterweights And Eases Bearing Loads. Air Squared Believes The Proposed Cssp Is A Perfect Fit In Support Of Methane In-Space Propulsion.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,216.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21P1977
- Development Unit For In-Space Pneumatic Helium Transfer Compressor
- 4 Oct 2022
- Development Unit For In-Space Pneumatic Helium Transfer Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $178,296.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0050
- The Proposed Innovation Supports Technologies For In Situ Resource Utilization (Isru) Processes By Collecting And Pressurizing Gasses From The Mars Atmosphere For Eventual Oxygen Production By Use Of Solid Oxide Electrolysis (Soxe). There Are Several Ways To Capture And Pressurize Co2, Including Freezing At Cryogenic Temperatures, Mechanical Compression, And Absorption. Completed Studies On Each Approach, Have Generally Favored Cryogenic Temperature And Mechanical Compression Solutions. Recently, Mechanical Compression Has Gained Momentum Through The Mars Oxygen Isru Experiment (Moxie), Which Utilizes An Air Squared Compressor For Mechanical Compression Of Co2. If This Approach Is Pursued Further For A Larger System, There Are Still Several Questions Concerning Reliability Over 10,000 Hours Of Autonomous Operation In Mars Environment And Scalability. Air Squared Plans On Addressing These Issues As Part Of Phase Ii.
- 5 Jul 2019
- The Proposed Innovation Supports Technologies For In Situ Resource Utilization (Isru) Processes By Collecting And Pressurizing Gasses From The Mars Atmosphere For Eventual Oxygen Production By Use Of Solid Oxide Electrolysis (Soxe). There Are Several Ways To Capture And Pressurize Co2, Including Freezing At Cryogenic Temperatures, Mechanical Compression, And Absorption. Completed Studies On Each Approach, Have Generally Favored Cryogenic Temperature And Mechanical Compression Solutions. Recently, Mechanical Compression Has Gained Momentum Through The Mars Oxygen Isru Experiment (Moxie), Which Utilizes An Air Squared Compressor For Mechanical Compression Of Co2. If This Approach Is Pursued Further For A Larger System, There Are Still Several Questions Concerning Reliability Over 10,000 Hours Of Autonomous Operation In Mars Environment And Scalability. Air Squared Plans On Addressing These Issues As Part Of Phase Ii.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $753,136.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21P1977
- Development Unit For In-Space Pneumatic Helium Transfer Compressor
- 13 Jul 2021
- Development Unit For In-Space Pneumatic Helium Transfer Compressor
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $178,296.00
- National Aeronautics And Space Administration (Nasa)
- N6833518C0567
- Igf::Ot::Igf Sbir Phase I
- 7 Jun 2018
- Igf::Ot::Igf Sbir Phase I
- Navair Warfare Ctr Aircraft Div Lke
- Department Of Defense (Dod)
- $124,975.00
- Department Of Defense (Dod)
- 80NSSC18C0050
- The Proposed Innovation Supports Technologies For In Situ Resource Utilization (Isru) Processes By Collecting And Pressurizing Gasses From The Mars Atmosphere For Eventual Oxygen Production By Use Of Solid Oxide Electrolysis (Soxe). There Are Several Ways To Capture And Pressurize Co2, Including Freezing At Cryogenic Temperatures, Mechanical Compression, And Absorption. Completed Studies On Each Approach, Have Generally Favored Cryogenic Temperature And Mechanical Compression Solutions. Recently, Mechanical Compression Has Gained Momentum Through The Mars Oxygen Isru Experiment (Moxie), Which Utilizes An Air Squared Compressor For Mechanical Compression Of Co2. If This Approach Is Pursued Further For A Larger System, There Are Still Several Questions Concerning Reliability Over 10,000 Hours Of Autonomous Operation In Mars Environment And Scalability. Air Squared Plans On Addressing These Issues As Part Of Phase Ii.
- 26 Jun 2020
- The Proposed Innovation Supports Technologies For In Situ Resource Utilization (Isru) Processes By Collecting And Pressurizing Gasses From The Mars Atmosphere For Eventual Oxygen Production By Use Of Solid Oxide Electrolysis (Soxe). There Are Several Ways To Capture And Pressurize Co2, Including Freezing At Cryogenic Temperatures, Mechanical Compression, And Absorption. Completed Studies On Each Approach, Have Generally Favored Cryogenic Temperature And Mechanical Compression Solutions. Recently, Mechanical Compression Has Gained Momentum Through The Mars Oxygen Isru Experiment (Moxie), Which Utilizes An Air Squared Compressor For Mechanical Compression Of Co2. If This Approach Is Pursued Further For A Larger System, There Are Still Several Questions Concerning Reliability Over 10,000 Hours Of Autonomous Operation In Mars Environment And Scalability. Air Squared Plans On Addressing These Issues As Part Of Phase Ii.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $753,136.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0204
- Nasa Seeks To Develop Novel Oxygen Extraction Concepts That Allow For The Production Of Oxygen On The Surface Of The.Moon Using Lunar Regolith.
- 19 May 2021
- Nasa Seeks To Develop Novel Oxygen Extraction Concepts That Allow For The Production Of Oxygen On The Surface Of The.Moon Using Lunar Regolith.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $124,948.00
- National Aeronautics And Space Administration (Nasa)