Blue Sun Enterprises, Inc.
CAGE Code: 49FB5
NCAGE Code: 49FB5
Status: Active
Type: Commercial Supplier
Dun & Bradstreet (DUNS): 361720787
Summary
Blue Sun Enterprises, Inc. is an Active Commercial Supplier with the Cage Code 49FB5 and is tracked by Dun & Bradstreet under DUNS Number 361720787..
Address
1942 Broadway Ste 317
Boulder CO 80302-5233
United States
Points of Contact
No Points of Contact...
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Frequently Asked Questions (FAQ) for CAGE 49FB5
- What is CAGE Code 49FB5?
- 49FB5 is the unique identifier used by NATO Organizations to reference the physical entity known as Blue Sun Enterprises, Inc. located at 1942 Broadway Ste 317, Boulder CO 80302-5233, United States.
- Who is CAGE Code 49FB5?
- 49FB5 refers to Blue Sun Enterprises, Inc. located at 1942 Broadway Ste 317, Boulder CO 80302-5233, United States.
- Where is CAGE Code 49FB5 Located?
- CAGE Code 49FB5 is located in Boulder, CO, USA.
Contracting History for CAGE 49FB5 Most Recent 25 Records
- 80NSSC18C0043
- The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is To Be Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (Iris, Ust) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money Potential Nasa Commercial Applications (Limit 1500 Characters, Approximately 150 Words) Autonav Mark 4 Is Applicable To Any Space Mission Requiring Any Of The Following: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Sbir-17-2-S3.04-8513 | Abstract - Autonav Mark 4: Autonomous Navig... Https://Ehb8.Gsfc.Nasa.Gov/Sbir/Docs/Protected/Users/Rev-Sel/Formb?Propo... 1 Of 2 2/16/2018 9:12 Am Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking: Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Calc -Maneuver Calc -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calc All Mission Perform Many Of The Above Activities, Often Using Ground-Based Processes That Are Slow And Expensive. Commercialized On-Board Autonomous Navigation As Provided By Autonav Mark 4 Can Be Targeted At The Whole Range Of Leo, Geo, And Interplanetary Missions, Large And Small. Autonav Mark 4 For Low-Thrust Missions (Including Psyche And Next Mars Orbiter) Would Allow A Dramatic Reduction In Navigation And Trajectory Calculation Costs By Moving The Bulk Of These Activities Onboard. Long Missions Like These Would Incur Even Larger Savings Using An4 Than More Modest Missions. Autonav Mark 4 Is Directly Applicable To Jpl's Deep Space Positioning System. By Using A Commercialized Autonav, Jpl Would Avoid Most Development Costs, Providing Only New Algorithms From Its Navigation Section To Plug Into The Autonav Mark 4 Architecture. Human Spaceflight Could Use Autonav Mark 4 For Navigation And Trajectory Calculation In The Event Of Communications Failure, Allowing Safe Reentry The Atmosphere And Landing Without Ground Interaction.
- 4 Jun 2021
- The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is To Be Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (Iris, Ust) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money Potential Nasa Commercial Applications (Limit 1500 Characters, Approximately 150 Words) Autonav Mark 4 Is Applicable To Any Space Mission Requiring Any Of The Following: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Sbir-17-2-S3.04-8513 | Abstract - Autonav Mark 4: Autonomous Navig... Https://Ehb8.Gsfc.Nasa.Gov/Sbir/Docs/Protected/Users/Rev-Sel/Formb?Propo... 1 Of 2 2/16/2018 9:12 Am Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking: Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Calc -Maneuver Calc -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calc All Mission Perform Many Of The Above Activities, Often Using Ground-Based Processes That Are Slow And Expensive. Commercialized On-Board Autonomous Navigation As Provided By Autonav Mark 4 Can Be Targeted At The Whole Range Of Leo, Geo, And Interplanetary Missions, Large And Small. Autonav Mark 4 For Low-Thrust Missions (Including Psyche And Next Mars Orbiter) Would Allow A Dramatic Reduction In Navigation And Trajectory Calculation Costs By Moving The Bulk Of These Activities Onboard. Long Missions Like These Would Incur Even Larger Savings Using An4 Than More Modest Missions. Autonav Mark 4 Is Directly Applicable To Jpl's Deep Space Positioning System. By Using A Commercialized Autonav, Jpl Would Avoid Most Development Costs, Providing Only New Algorithms From Its Navigation Section To Plug Into The Autonav Mark 4 Architecture. Human Spaceflight Could Use Autonav Mark 4 For Navigation And Trajectory Calculation In The Event Of Communications Failure, Allowing Safe Reentry The Atmosphere And Landing Without Ground Interaction.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,568.00
- National Aeronautics And Space Administration (Nasa)
- NNX15CK02C
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- 5 Jun 2018
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,247,012.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- E014042 Virtual Machine Language Consultation
- 9 May 2023
- E014042 Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $321,506.00
- National Aeronautics And Space Administration (Nasa)
- NNX17CP77P
- Igf::Ot::Igf The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (E.G. Iris) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money.
- 8 Jun 2017
- Igf::Ot::Igf The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (E.G. Iris) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $122,700.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- Eo14042 Virtual Machine Language Consultation
- 10 Jan 2023
- Eo14042 Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $321,506.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- Eo14042 Virtual Machine Language Consultation
- 1 Feb 2022
- Eo14042 Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $225,806.00
- National Aeronautics And Space Administration (Nasa)
- NNX15CK02C
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- 1 May 2018
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,247,012.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- Virtual Machine Language Consultation
- 18 Dec 2023
- Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $321,506.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0043
- The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is To Be Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (Iris, Ust) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money Potential Nasa Commercial Applications (Limit 1500 Characters, Approximately 150 Words) Autonav Mark 4 Is Applicable To Any Space Mission Requiring Any Of The Following: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Sbir-17-2-S3.04-8513 | Abstract - Autonav Mark 4: Autonomous Navig... Https://Ehb8.Gsfc.Nasa.Gov/Sbir/Docs/Protected/Users/Rev-Sel/Formb?Propo... 1 Of 2 2/16/2018 9:12 Am Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking: Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Calc -Maneuver Calc -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calc All Mission Perform Many Of The Above Activities, Often Using Ground-Based Processes That Are Slow And Expensive. Commercialized On-Board Autonomous Navigation As Provided By Autonav Mark 4 Can Be Targeted At The Whole Range Of Leo, Geo, And Interplanetary Missions, Large And Small. Autonav Mark 4 For Low-Thrust Missions (Including Psyche And Next Mars Orbiter) Would Allow A Dramatic Reduction In Navigation And Trajectory Calculation Costs By Moving The Bulk Of These Activities Onboard. Long Missions Like These Would Incur Even Larger Savings Using An4 Than More Modest Missions. Autonav Mark 4 Is Directly Applicable To Jpl's Deep Space Positioning System. By Using A Commercialized Autonav, Jpl Would Avoid Most Development Costs, Providing Only New Algorithms From Its Navigation Section To Plug Into The Autonav Mark 4 Architecture. Human Spaceflight Could Use Autonav Mark 4 For Navigation And Trajectory Calculation In The Event Of Communications Failure, Allowing Safe Reentry The Atmosphere And Landing Without Ground Interaction.
- 21 Apr 2020
- The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is To Be Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (Iris, Ust) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money Potential Nasa Commercial Applications (Limit 1500 Characters, Approximately 150 Words) Autonav Mark 4 Is Applicable To Any Space Mission Requiring Any Of The Following: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Sbir-17-2-S3.04-8513 | Abstract - Autonav Mark 4: Autonomous Navig... Https://Ehb8.Gsfc.Nasa.Gov/Sbir/Docs/Protected/Users/Rev-Sel/Formb?Propo... 1 Of 2 2/16/2018 9:12 Am Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking: Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Calc -Maneuver Calc -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calc All Mission Perform Many Of The Above Activities, Often Using Ground-Based Processes That Are Slow And Expensive. Commercialized On-Board Autonomous Navigation As Provided By Autonav Mark 4 Can Be Targeted At The Whole Range Of Leo, Geo, And Interplanetary Missions, Large And Small. Autonav Mark 4 For Low-Thrust Missions (Including Psyche And Next Mars Orbiter) Would Allow A Dramatic Reduction In Navigation And Trajectory Calculation Costs By Moving The Bulk Of These Activities Onboard. Long Missions Like These Would Incur Even Larger Savings Using An4 Than More Modest Missions. Autonav Mark 4 Is Directly Applicable To Jpl's Deep Space Positioning System. By Using A Commercialized Autonav, Jpl Would Avoid Most Development Costs, Providing Only New Algorithms From Its Navigation Section To Plug Into The Autonav Mark 4 Architecture. Human Spaceflight Could Use Autonav Mark 4 For Navigation And Trajectory Calculation In The Event Of Communications Failure, Allowing Safe Reentry The Atmosphere And Landing Without Ground Interaction.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,568.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- Virtual Machine Language Consultation
- 18 Aug 2021
- Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $81,058.00
- National Aeronautics And Space Administration (Nasa)
- NNX15CK02C
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- 7 Dec 2018
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,637,830.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- Virtual Machine Language Consultation
- 26 Aug 2021
- Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $81,058.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC18C0043
- The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is To Be Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (Iris, Ust) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money Potential Nasa Commercial Applications (Limit 1500 Characters, Approximately 150 Words) Autonav Mark 4 Is Applicable To Any Space Mission Requiring Any Of The Following: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Sbir-17-2-S3.04-8513 | Abstract - Autonav Mark 4: Autonomous Navig... Https://Ehb8.Gsfc.Nasa.Gov/Sbir/Docs/Protected/Users/Rev-Sel/Formb?Propo... 1 Of 2 2/16/2018 9:12 Am Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking: Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Calc -Maneuver Calc -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calc All Mission Perform Many Of The Above Activities, Often Using Ground-Based Processes That Are Slow And Expensive. Commercialized On-Board Autonomous Navigation As Provided By Autonav Mark 4 Can Be Targeted At The Whole Range Of Leo, Geo, And Interplanetary Missions, Large And Small. Autonav Mark 4 For Low-Thrust Missions (Including Psyche And Next Mars Orbiter) Would Allow A Dramatic Reduction In Navigation And Trajectory Calculation Costs By Moving The Bulk Of These Activities Onboard. Long Missions Like These Would Incur Even Larger Savings Using An4 Than More Modest Missions. Autonav Mark 4 Is Directly Applicable To Jpl's Deep Space Positioning System. By Using A Commercialized Autonav, Jpl Would Avoid Most Development Costs, Providing Only New Algorithms From Its Navigation Section To Plug Into The Autonav Mark 4 Architecture. Human Spaceflight Could Use Autonav Mark 4 For Navigation And Trajectory Calculation In The Event Of Communications Failure, Allowing Safe Reentry The Atmosphere And Landing Without Ground Interaction.
- 3 Jun 2018
- The Growing Number Of Missions In Deep Space, From Discovery Class Missions Like Psyche And Lucy Down To Very Small Spacecraft Like Lunar Flashlight, Is Driving The Need For Standardized, Flexible, Full-Featured Flight Software For Spacecraft Guidance, Navigation, And Control (Gnc). Autonomous Gnc Allows A Spacecraft To Perform Most Of Its Own Navigation Activities Without The Need For Ground-Based Personnel And Dsn Time, Reducing Cost And Required Dsn Contact Time, Saving Money, And Allowing Specialized Navigation Personnel From Different Nasa Centers To Be Easily Shared Among Missions. Autonomous Gnc Activities Include: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking Of Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Derivation -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calculations Autonav From The Jet Propulsion Laboratory Implements These Functions, And Components Have Flown On Deep Space 1 And Deep Impact. With An Appropriate Application Of Software Development Process To Reengineer The Code, A New Autonav Mark 4 Could Be Made Available As A Commercialized Product Meeting Nasa Class B Software Standards, Thereby Enabling Its Easy Inclusion On A Wide Variety Of Nasa And Non-Nasa Missions. Autonav Mark 4 Source Code Is To Be Designed And Tested To Be Compatible With A Variety Of Different Cpus (E.G. Sparc, Ppc, Intel), Real-Time Operating Systems (Vxworks, Rtems), And Flight Software Cores Like Nasa Core Flight System. This Approach Allows An4 To Be Deployed In The Widest-Possible Set Of Environments: -Within Strs-Compatible Space Radios (Iris, Ust) -In The Flight Software Load Of The Spacecraft C&Dh -In A Dedicated Stand-Alone Instrument Like The Deep Space Positioning System Autonav Mark 4 Provides Highly Capable Autonomous Gnc While Saving Missions Money Potential Nasa Commercial Applications (Limit 1500 Characters, Approximately 150 Words) Autonav Mark 4 Is Applicable To Any Space Mission Requiring Any Of The Following: -Spacecraft Positioning Absolute And Relative (Helio, Planet, Small-Body) Sbir-17-2-S3.04-8513 | Abstract - Autonav Mark 4: Autonomous Navig... Https://Ehb8.Gsfc.Nasa.Gov/Sbir/Docs/Protected/Users/Rev-Sel/Formb?Propo... 1 Of 2 2/16/2018 9:12 Am Relative To Small Bodies, Other Spacecraft For Rendezvous -Orbit Determination -Target Tracking: Bodies, Apertures, Spacecraft, Ground-Based Assets -Trajectory Calc -Maneuver Calc -Low-Thrust Maneuvering For Solar Electric Propulsion (Sep) -Ephemeris Calc All Mission Perform Many Of The Above Activities, Often Using Ground-Based Processes That Are Slow And Expensive. Commercialized On-Board Autonomous Navigation As Provided By Autonav Mark 4 Can Be Targeted At The Whole Range Of Leo, Geo, And Interplanetary Missions, Large And Small. Autonav Mark 4 For Low-Thrust Missions (Including Psyche And Next Mars Orbiter) Would Allow A Dramatic Reduction In Navigation And Trajectory Calculation Costs By Moving The Bulk Of These Activities Onboard. Long Missions Like These Would Incur Even Larger Savings Using An4 Than More Modest Missions. Autonav Mark 4 Is Directly Applicable To Jpl's Deep Space Positioning System. By Using A Commercialized Autonav, Jpl Would Avoid Most Development Costs, Providing Only New Algorithms From Its Navigation Section To Plug Into The Autonav Mark 4 Architecture. Human Spaceflight Could Use Autonav Mark 4 For Navigation And Trajectory Calculation In The Event Of Communications Failure, Allowing Safe Reentry The Atmosphere And Landing Without Ground Interaction.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $749,568.00
- National Aeronautics And Space Administration (Nasa)
- 80NSSC21C0599
- Virtual Machine Language Consultation
- 11 Oct 2023
- Virtual Machine Language Consultation
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $321,506.00
- National Aeronautics And Space Administration (Nasa)
- NNX15CK02C
- The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around
- 7 Aug 2020
- The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,733,365.00
- National Aeronautics And Space Administration (Nasa)
- NNX15CK02C
- The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around
- 30 Sep 2019
- The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,637,830.00
- National Aeronautics And Space Administration (Nasa)
- NNX15CK02C
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- 29 Oct 2018
- Igf::Ot::Igf The Primary Objective Of The Resolve Mission Is To Verify The Presence Of Water And Other Volatiles On The Lunar Surface By Direct, Ground-Truth Measurements And To Serve As A Precursor For Future Prospecting Missions To A Variety Of Locations Around The Solar System. The Resolve Mission Shall Focus On Exploring Lunar Regolith In And/Or Around Permanently Shadowed Polar-Regions Of The Moon. The Objective Has Been Further Refined To Include: Determination Of The Form, Concentration, And Spatial Distribution Of Hydrogen And Other Volatiles Inside And/Or Outside Of Shadowed Lunar Polar Regions To A Depth Of At Least 1 M. Determination Of Bulk Properties Of Lunar Material Inside And Outside Of Shadowed Lunar Polar Regions. Demonstration Of Regolith Prospecting, Extraction, And Processing Operations In The Lunar Environment. Demonstration Of Oxygen (Water) Extraction From Regolith Via Hydrogen Reduction In The Lunar Environment.
- Nasa Shared Services Center
- National Aeronautics And Space Administration (Nasa)
- $1,247,012.00
- National Aeronautics And Space Administration (Nasa)