ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation
Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Stelzl, Daniel [verfasserIn] Pfeiffer, Ernst K. [verfasserIn] Hemme, Hugo Garcia [verfasserIn] Lindenmaier, Peter [verfasserIn] Riemer, Arne [verfasserIn] Cubillo, Alba Alegre [verfasserIn] Spröwitz, Tom [verfasserIn] Seefeldt, Patric [verfasserIn] Meyer, Sebastian [verfasserIn] Zander, Martin [verfasserIn] Bunte, Karl Dietrich [verfasserIn] Miller, Anatoli [verfasserIn] Weikert, Sven [verfasserIn] Meier, Stefan [verfasserIn] Koch, Michael [verfasserIn] Lender, Stefan [verfasserIn] Vogt, Cornelius [verfasserIn] Ernst, Ruwan [verfasserIn] Schmid, Michael [verfasserIn] Cardone, Tiziana [verfasserIn] Smet, Geert [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2021 |
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| Schlagwörter: |
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| Anmerkung: |
© CEAS 2021 |
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| Übergeordnetes Werk: |
Enthalten in: CEAS space journal - Wien [u.a.] : Springer, 2011, 13(2021), 4 vom: 24. März, Seite 591-598 |
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| Übergeordnetes Werk: |
volume:13 ; year:2021 ; number:4 ; day:24 ; month:03 ; pages:591-598 |
| Links: |
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| DOI / URN: |
10.1007/s12567-021-00355-7 |
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| Katalog-ID: |
SPR04500918X |
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| 520 | |a Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). | ||
| 650 | 4 | |a Passive De-orbit |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a CleanGreen Space Mission |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Dragsail |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Cleanspace |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Space Debris Mitigation |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Reference Mission |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Proto Flight Model |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Pfeiffer, Ernst K. |e verfasserin |4 aut | |
| 700 | 1 | |a Hemme, Hugo Garcia |e verfasserin |4 aut | |
| 700 | 1 | |a Lindenmaier, Peter |e verfasserin |4 aut | |
| 700 | 1 | |a Riemer, Arne |e verfasserin |4 aut | |
| 700 | 1 | |a Cubillo, Alba Alegre |e verfasserin |4 aut | |
| 700 | 1 | |a Spröwitz, Tom |e verfasserin |4 aut | |
| 700 | 1 | |a Seefeldt, Patric |e verfasserin |4 aut | |
| 700 | 1 | |a Meyer, Sebastian |e verfasserin |4 aut | |
| 700 | 1 | |a Zander, Martin |e verfasserin |4 aut | |
| 700 | 1 | |a Bunte, Karl Dietrich |e verfasserin |4 aut | |
| 700 | 1 | |a Miller, Anatoli |e verfasserin |4 aut | |
| 700 | 1 | |a Weikert, Sven |e verfasserin |4 aut | |
| 700 | 1 | |a Meier, Stefan |e verfasserin |4 aut | |
| 700 | 1 | |a Koch, Michael |e verfasserin |4 aut | |
| 700 | 1 | |a Lender, Stefan |e verfasserin |4 aut | |
| 700 | 1 | |a Vogt, Cornelius |e verfasserin |4 aut | |
| 700 | 1 | |a Ernst, Ruwan |e verfasserin |4 aut | |
| 700 | 1 | |a Schmid, Michael |e verfasserin |4 aut | |
| 700 | 1 | |a Cardone, Tiziana |e verfasserin |4 aut | |
| 700 | 1 | |a Smet, Geert |e verfasserin |4 aut | |
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10.1007/s12567-021-00355-7 doi (DE-627)SPR04500918X (SPR)s12567-021-00355-7-e DE-627 ger DE-627 rakwb eng 620 ASE Stelzl, Daniel verfasserin aut ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © CEAS 2021 Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). Passive De-orbit (dpeaa)DE-He213 CleanGreen Space Mission (dpeaa)DE-He213 Dragsail (dpeaa)DE-He213 Cleanspace (dpeaa)DE-He213 Space Debris Mitigation (dpeaa)DE-He213 Reference Mission (dpeaa)DE-He213 Proto Flight Model (dpeaa)DE-He213 Pfeiffer, Ernst K. verfasserin aut Hemme, Hugo Garcia verfasserin aut Lindenmaier, Peter verfasserin aut Riemer, Arne verfasserin aut Cubillo, Alba Alegre verfasserin aut Spröwitz, Tom verfasserin aut Seefeldt, Patric verfasserin aut Meyer, Sebastian verfasserin aut Zander, Martin verfasserin aut Bunte, Karl Dietrich verfasserin aut Miller, Anatoli verfasserin aut Weikert, Sven verfasserin aut Meier, Stefan verfasserin aut Koch, Michael verfasserin aut Lender, Stefan verfasserin aut Vogt, Cornelius verfasserin aut Ernst, Ruwan verfasserin aut Schmid, Michael verfasserin aut Cardone, Tiziana verfasserin aut Smet, Geert verfasserin aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 13(2021), 4 vom: 24. März, Seite 591-598 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:13 year:2021 number:4 day:24 month:03 pages:591-598 https://dx.doi.org/10.1007/s12567-021-00355-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2021 4 24 03 591-598 |
| spelling |
10.1007/s12567-021-00355-7 doi (DE-627)SPR04500918X (SPR)s12567-021-00355-7-e DE-627 ger DE-627 rakwb eng 620 ASE Stelzl, Daniel verfasserin aut ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © CEAS 2021 Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). Passive De-orbit (dpeaa)DE-He213 CleanGreen Space Mission (dpeaa)DE-He213 Dragsail (dpeaa)DE-He213 Cleanspace (dpeaa)DE-He213 Space Debris Mitigation (dpeaa)DE-He213 Reference Mission (dpeaa)DE-He213 Proto Flight Model (dpeaa)DE-He213 Pfeiffer, Ernst K. verfasserin aut Hemme, Hugo Garcia verfasserin aut Lindenmaier, Peter verfasserin aut Riemer, Arne verfasserin aut Cubillo, Alba Alegre verfasserin aut Spröwitz, Tom verfasserin aut Seefeldt, Patric verfasserin aut Meyer, Sebastian verfasserin aut Zander, Martin verfasserin aut Bunte, Karl Dietrich verfasserin aut Miller, Anatoli verfasserin aut Weikert, Sven verfasserin aut Meier, Stefan verfasserin aut Koch, Michael verfasserin aut Lender, Stefan verfasserin aut Vogt, Cornelius verfasserin aut Ernst, Ruwan verfasserin aut Schmid, Michael verfasserin aut Cardone, Tiziana verfasserin aut Smet, Geert verfasserin aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 13(2021), 4 vom: 24. März, Seite 591-598 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:13 year:2021 number:4 day:24 month:03 pages:591-598 https://dx.doi.org/10.1007/s12567-021-00355-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2021 4 24 03 591-598 |
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10.1007/s12567-021-00355-7 doi (DE-627)SPR04500918X (SPR)s12567-021-00355-7-e DE-627 ger DE-627 rakwb eng 620 ASE Stelzl, Daniel verfasserin aut ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © CEAS 2021 Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). Passive De-orbit (dpeaa)DE-He213 CleanGreen Space Mission (dpeaa)DE-He213 Dragsail (dpeaa)DE-He213 Cleanspace (dpeaa)DE-He213 Space Debris Mitigation (dpeaa)DE-He213 Reference Mission (dpeaa)DE-He213 Proto Flight Model (dpeaa)DE-He213 Pfeiffer, Ernst K. verfasserin aut Hemme, Hugo Garcia verfasserin aut Lindenmaier, Peter verfasserin aut Riemer, Arne verfasserin aut Cubillo, Alba Alegre verfasserin aut Spröwitz, Tom verfasserin aut Seefeldt, Patric verfasserin aut Meyer, Sebastian verfasserin aut Zander, Martin verfasserin aut Bunte, Karl Dietrich verfasserin aut Miller, Anatoli verfasserin aut Weikert, Sven verfasserin aut Meier, Stefan verfasserin aut Koch, Michael verfasserin aut Lender, Stefan verfasserin aut Vogt, Cornelius verfasserin aut Ernst, Ruwan verfasserin aut Schmid, Michael verfasserin aut Cardone, Tiziana verfasserin aut Smet, Geert verfasserin aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 13(2021), 4 vom: 24. März, Seite 591-598 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:13 year:2021 number:4 day:24 month:03 pages:591-598 https://dx.doi.org/10.1007/s12567-021-00355-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2021 4 24 03 591-598 |
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10.1007/s12567-021-00355-7 doi (DE-627)SPR04500918X (SPR)s12567-021-00355-7-e DE-627 ger DE-627 rakwb eng 620 ASE Stelzl, Daniel verfasserin aut ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © CEAS 2021 Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). Passive De-orbit (dpeaa)DE-He213 CleanGreen Space Mission (dpeaa)DE-He213 Dragsail (dpeaa)DE-He213 Cleanspace (dpeaa)DE-He213 Space Debris Mitigation (dpeaa)DE-He213 Reference Mission (dpeaa)DE-He213 Proto Flight Model (dpeaa)DE-He213 Pfeiffer, Ernst K. verfasserin aut Hemme, Hugo Garcia verfasserin aut Lindenmaier, Peter verfasserin aut Riemer, Arne verfasserin aut Cubillo, Alba Alegre verfasserin aut Spröwitz, Tom verfasserin aut Seefeldt, Patric verfasserin aut Meyer, Sebastian verfasserin aut Zander, Martin verfasserin aut Bunte, Karl Dietrich verfasserin aut Miller, Anatoli verfasserin aut Weikert, Sven verfasserin aut Meier, Stefan verfasserin aut Koch, Michael verfasserin aut Lender, Stefan verfasserin aut Vogt, Cornelius verfasserin aut Ernst, Ruwan verfasserin aut Schmid, Michael verfasserin aut Cardone, Tiziana verfasserin aut Smet, Geert verfasserin aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 13(2021), 4 vom: 24. März, Seite 591-598 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:13 year:2021 number:4 day:24 month:03 pages:591-598 https://dx.doi.org/10.1007/s12567-021-00355-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2021 4 24 03 591-598 |
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10.1007/s12567-021-00355-7 doi (DE-627)SPR04500918X (SPR)s12567-021-00355-7-e DE-627 ger DE-627 rakwb eng 620 ASE Stelzl, Daniel verfasserin aut ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation 2021 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © CEAS 2021 Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). Passive De-orbit (dpeaa)DE-He213 CleanGreen Space Mission (dpeaa)DE-He213 Dragsail (dpeaa)DE-He213 Cleanspace (dpeaa)DE-He213 Space Debris Mitigation (dpeaa)DE-He213 Reference Mission (dpeaa)DE-He213 Proto Flight Model (dpeaa)DE-He213 Pfeiffer, Ernst K. verfasserin aut Hemme, Hugo Garcia verfasserin aut Lindenmaier, Peter verfasserin aut Riemer, Arne verfasserin aut Cubillo, Alba Alegre verfasserin aut Spröwitz, Tom verfasserin aut Seefeldt, Patric verfasserin aut Meyer, Sebastian verfasserin aut Zander, Martin verfasserin aut Bunte, Karl Dietrich verfasserin aut Miller, Anatoli verfasserin aut Weikert, Sven verfasserin aut Meier, Stefan verfasserin aut Koch, Michael verfasserin aut Lender, Stefan verfasserin aut Vogt, Cornelius verfasserin aut Ernst, Ruwan verfasserin aut Schmid, Michael verfasserin aut Cardone, Tiziana verfasserin aut Smet, Geert verfasserin aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 13(2021), 4 vom: 24. März, Seite 591-598 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:13 year:2021 number:4 day:24 month:03 pages:591-598 https://dx.doi.org/10.1007/s12567-021-00355-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 13 2021 4 24 03 591-598 |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR04500918X</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220111133636.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">210907s2021 xx |||||o 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s12567-021-00355-7</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR04500918X</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s12567-021-00355-7-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">620</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Stelzl, Daniel</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2021</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© CEAS 2021</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. 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|
| author |
Stelzl, Daniel |
| spellingShingle |
Stelzl, Daniel ddc 620 misc Passive De-orbit misc CleanGreen Space Mission misc Dragsail misc Cleanspace misc Space Debris Mitigation misc Reference Mission misc Proto Flight Model ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation |
| authorStr |
Stelzl, Daniel |
| ppnlink_with_tag_str_mv |
@@773@@(DE-627)626054389 |
| format |
electronic Article |
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620 - Engineering & allied operations |
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Stelzl, Daniel Pfeiffer, Ernst K. Hemme, Hugo Garcia Lindenmaier, Peter Riemer, Arne Cubillo, Alba Alegre Spröwitz, Tom Seefeldt, Patric Meyer, Sebastian Zander, Martin Bunte, Karl Dietrich Miller, Anatoli Weikert, Sven Meier, Stefan Koch, Michael Lender, Stefan Vogt, Cornelius Ernst, Ruwan Schmid, Michael Cardone, Tiziana Smet, Geert |
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Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). © CEAS 2021 |
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Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). © CEAS 2021 |
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Abstract The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up “In Orbit Demonstration” (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called “watchdog routine” inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called “100% passive”, a “CleanGreen Space Mission”. First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE). © CEAS 2021 |
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| score |
7.3984203 |