Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)

Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. Wh...
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Autor*in:	Vaidya, S. [verfasserIn] Traub, C. Romano, F. Herdrich, G. H. Chan, Y.-A. Fasoulas, S. Roberts, P. C. E. Crisp, N. H. Edmondson, S. Haigh, S. J. Holmes, B. E. A. Macario-Rojas, A. Oiko, V. T. A. Smith, K. L. Sinpetru, L. A. Becedas, J. Sulliotti-Linner, V. Christensen, S. Hanessian, V. Jensen, T. K. Nielsen, J. Bisgaard, M. Garcia-Almiñana, D. Rodriguez-Donaire, S. Suerda, M. Garcia-Berenguer, M. Kataria, D. Villain, R. Seminari, S. Conte, A. Belkouchi, B.

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2022

Schlagwörter:	Very Low Earth Orbit Very Low Mars Orbit Atmosphere-Breathing Electric Propulsion Earth observation Space tug

Anmerkung:	© The Author(s), under exclusive licence to Council of European Aerospace Societies 2022

Übergeordnetes Werk:	Enthalten in: CEAS space journal - Wien [u.a.] : Springer, 2011, 14(2022), 4 vom: 21. März, Seite 689-706
Übergeordnetes Werk:	volume:14 ; year:2022 ; number:4 ; day:21 ; month:03 ; pages:689-706

Links:	Volltext

DOI / URN:	10.1007/s12567-022-00436-1

Katalog-ID:	SPR048168106

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520			\|a Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications.
650		4	\|a Very Low Earth Orbit \|7 (dpeaa)DE-He213
650		4	\|a Very Low Mars Orbit \|7 (dpeaa)DE-He213
650		4	\|a Atmosphere-Breathing Electric Propulsion \|7 (dpeaa)DE-He213
650		4	\|a Earth observation \|7 (dpeaa)DE-He213
650		4	\|a Space tug \|7 (dpeaa)DE-He213
700	1		\|a Traub, C. \|4 aut
700	1		\|a Romano, F. \|4 aut
700	1		\|a Herdrich, G. H. \|4 aut
700	1		\|a Chan, Y.-A. \|4 aut
700	1		\|a Fasoulas, S. \|4 aut
700	1		\|a Roberts, P. C. E. \|4 aut
700	1		\|a Crisp, N. H. \|4 aut
700	1		\|a Edmondson, S. \|4 aut
700	1		\|a Haigh, S. J. \|4 aut
700	1		\|a Holmes, B. E. A. \|4 aut
700	1		\|a Macario-Rojas, A. \|4 aut
700	1		\|a Oiko, V. T. A. \|4 aut
700	1		\|a Smith, K. L. \|4 aut
700	1		\|a Sinpetru, L. A. \|4 aut
700	1		\|a Becedas, J. \|4 aut
700	1		\|a Sulliotti-Linner, V. \|4 aut
700	1		\|a Christensen, S. \|4 aut
700	1		\|a Hanessian, V. \|4 aut
700	1		\|a Jensen, T. K. \|4 aut
700	1		\|a Nielsen, J. \|4 aut
700	1		\|a Bisgaard, M. \|4 aut
700	1		\|a Garcia-Almiñana, D. \|4 aut
700	1		\|a Rodriguez-Donaire, S. \|4 aut
700	1		\|a Suerda, M. \|4 aut
700	1		\|a Garcia-Berenguer, M. \|4 aut
700	1		\|a Kataria, D. \|4 aut
700	1		\|a Villain, R. \|4 aut
700	1		\|a Seminari, S. \|4 aut
700	1		\|a Conte, A. \|4 aut
700	1		\|a Belkouchi, B. \|4 aut
773	0	8	\|i Enthalten in \|t CEAS space journal \|d Wien [u.a.] : Springer, 2011 \|g 14(2022), 4 vom: 21. März, Seite 689-706 \|w (DE-627)626054389 \|w (DE-600)2553331-9 \|x 1868-2510 \|7 nnns
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952			\|d 14 \|j 2022 \|e 4 \|b 21 \|c 03 \|h 689-706

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allfields	10.1007/s12567-022-00436-1 doi (DE-627)SPR048168106 (SPR)s12567-022-00436-1-e DE-627 ger DE-627 rakwb eng Vaidya, S. verfasserin (orcid)0000-0002-9927-919X aut Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP) 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022 Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. Very Low Earth Orbit (dpeaa)DE-He213 Very Low Mars Orbit (dpeaa)DE-He213 Atmosphere-Breathing Electric Propulsion (dpeaa)DE-He213 Earth observation (dpeaa)DE-He213 Space tug (dpeaa)DE-He213 Traub, C. aut Romano, F. aut Herdrich, G. H. aut Chan, Y.-A. aut Fasoulas, S. aut Roberts, P. C. E. aut Crisp, N. H. aut Edmondson, S. aut Haigh, S. J. aut Holmes, B. E. A. aut Macario-Rojas, A. aut Oiko, V. T. A. aut Smith, K. L. aut Sinpetru, L. A. aut Becedas, J. aut Sulliotti-Linner, V. aut Christensen, S. aut Hanessian, V. aut Jensen, T. K. aut Nielsen, J. aut Bisgaard, M. aut Garcia-Almiñana, D. aut Rodriguez-Donaire, S. aut Suerda, M. aut Garcia-Berenguer, M. aut Kataria, D. aut Villain, R. aut Seminari, S. aut Conte, A. aut Belkouchi, B. aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 14(2022), 4 vom: 21. März, Seite 689-706 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:14 year:2022 number:4 day:21 month:03 pages:689-706 https://dx.doi.org/10.1007/s12567-022-00436-1 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 14 2022 4 21 03 689-706
spelling	10.1007/s12567-022-00436-1 doi (DE-627)SPR048168106 (SPR)s12567-022-00436-1-e DE-627 ger DE-627 rakwb eng Vaidya, S. verfasserin (orcid)0000-0002-9927-919X aut Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP) 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022 Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. Very Low Earth Orbit (dpeaa)DE-He213 Very Low Mars Orbit (dpeaa)DE-He213 Atmosphere-Breathing Electric Propulsion (dpeaa)DE-He213 Earth observation (dpeaa)DE-He213 Space tug (dpeaa)DE-He213 Traub, C. aut Romano, F. aut Herdrich, G. H. aut Chan, Y.-A. aut Fasoulas, S. aut Roberts, P. C. E. aut Crisp, N. H. aut Edmondson, S. aut Haigh, S. J. aut Holmes, B. E. A. aut Macario-Rojas, A. aut Oiko, V. T. A. aut Smith, K. L. aut Sinpetru, L. A. aut Becedas, J. aut Sulliotti-Linner, V. aut Christensen, S. aut Hanessian, V. aut Jensen, T. K. aut Nielsen, J. aut Bisgaard, M. aut Garcia-Almiñana, D. aut Rodriguez-Donaire, S. aut Suerda, M. aut Garcia-Berenguer, M. aut Kataria, D. aut Villain, R. aut Seminari, S. aut Conte, A. aut Belkouchi, B. aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 14(2022), 4 vom: 21. März, Seite 689-706 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:14 year:2022 number:4 day:21 month:03 pages:689-706 https://dx.doi.org/10.1007/s12567-022-00436-1 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 14 2022 4 21 03 689-706
allfields_unstemmed	10.1007/s12567-022-00436-1 doi (DE-627)SPR048168106 (SPR)s12567-022-00436-1-e DE-627 ger DE-627 rakwb eng Vaidya, S. verfasserin (orcid)0000-0002-9927-919X aut Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP) 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022 Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. Very Low Earth Orbit (dpeaa)DE-He213 Very Low Mars Orbit (dpeaa)DE-He213 Atmosphere-Breathing Electric Propulsion (dpeaa)DE-He213 Earth observation (dpeaa)DE-He213 Space tug (dpeaa)DE-He213 Traub, C. aut Romano, F. aut Herdrich, G. H. aut Chan, Y.-A. aut Fasoulas, S. aut Roberts, P. C. E. aut Crisp, N. H. aut Edmondson, S. aut Haigh, S. J. aut Holmes, B. E. A. aut Macario-Rojas, A. aut Oiko, V. T. A. aut Smith, K. L. aut Sinpetru, L. A. aut Becedas, J. aut Sulliotti-Linner, V. aut Christensen, S. aut Hanessian, V. aut Jensen, T. K. aut Nielsen, J. aut Bisgaard, M. aut Garcia-Almiñana, D. aut Rodriguez-Donaire, S. aut Suerda, M. aut Garcia-Berenguer, M. aut Kataria, D. aut Villain, R. aut Seminari, S. aut Conte, A. aut Belkouchi, B. aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 14(2022), 4 vom: 21. März, Seite 689-706 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:14 year:2022 number:4 day:21 month:03 pages:689-706 https://dx.doi.org/10.1007/s12567-022-00436-1 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 14 2022 4 21 03 689-706
allfieldsGer	10.1007/s12567-022-00436-1 doi (DE-627)SPR048168106 (SPR)s12567-022-00436-1-e DE-627 ger DE-627 rakwb eng Vaidya, S. verfasserin (orcid)0000-0002-9927-919X aut Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP) 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022 Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. Very Low Earth Orbit (dpeaa)DE-He213 Very Low Mars Orbit (dpeaa)DE-He213 Atmosphere-Breathing Electric Propulsion (dpeaa)DE-He213 Earth observation (dpeaa)DE-He213 Space tug (dpeaa)DE-He213 Traub, C. aut Romano, F. aut Herdrich, G. H. aut Chan, Y.-A. aut Fasoulas, S. aut Roberts, P. C. E. aut Crisp, N. H. aut Edmondson, S. aut Haigh, S. J. aut Holmes, B. E. A. aut Macario-Rojas, A. aut Oiko, V. T. A. aut Smith, K. L. aut Sinpetru, L. A. aut Becedas, J. aut Sulliotti-Linner, V. aut Christensen, S. aut Hanessian, V. aut Jensen, T. K. aut Nielsen, J. aut Bisgaard, M. aut Garcia-Almiñana, D. aut Rodriguez-Donaire, S. aut Suerda, M. aut Garcia-Berenguer, M. aut Kataria, D. aut Villain, R. aut Seminari, S. aut Conte, A. aut Belkouchi, B. aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 14(2022), 4 vom: 21. März, Seite 689-706 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:14 year:2022 number:4 day:21 month:03 pages:689-706 https://dx.doi.org/10.1007/s12567-022-00436-1 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 14 2022 4 21 03 689-706
allfieldsSound	10.1007/s12567-022-00436-1 doi (DE-627)SPR048168106 (SPR)s12567-022-00436-1-e DE-627 ger DE-627 rakwb eng Vaidya, S. verfasserin (orcid)0000-0002-9927-919X aut Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP) 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022 Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. Very Low Earth Orbit (dpeaa)DE-He213 Very Low Mars Orbit (dpeaa)DE-He213 Atmosphere-Breathing Electric Propulsion (dpeaa)DE-He213 Earth observation (dpeaa)DE-He213 Space tug (dpeaa)DE-He213 Traub, C. aut Romano, F. aut Herdrich, G. H. aut Chan, Y.-A. aut Fasoulas, S. aut Roberts, P. C. E. aut Crisp, N. H. aut Edmondson, S. aut Haigh, S. J. aut Holmes, B. E. A. aut Macario-Rojas, A. aut Oiko, V. T. A. aut Smith, K. L. aut Sinpetru, L. A. aut Becedas, J. aut Sulliotti-Linner, V. aut Christensen, S. aut Hanessian, V. aut Jensen, T. K. aut Nielsen, J. aut Bisgaard, M. aut Garcia-Almiñana, D. aut Rodriguez-Donaire, S. aut Suerda, M. aut Garcia-Berenguer, M. aut Kataria, D. aut Villain, R. aut Seminari, S. aut Conte, A. aut Belkouchi, B. aut Enthalten in CEAS space journal Wien [u.a.] : Springer, 2011 14(2022), 4 vom: 21. März, Seite 689-706 (DE-627)626054389 (DE-600)2553331-9 1868-2510 nnns volume:14 year:2022 number:4 day:21 month:03 pages:689-706 https://dx.doi.org/10.1007/s12567-022-00436-1 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 14 2022 4 21 03 689-706
language	English
source	Enthalten in CEAS space journal 14(2022), 4 vom: 21. März, Seite 689-706 volume:14 year:2022 number:4 day:21 month:03 pages:689-706
sourceStr	Enthalten in CEAS space journal 14(2022), 4 vom: 21. März, Seite 689-706 volume:14 year:2022 number:4 day:21 month:03 pages:689-706
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Very Low Earth Orbit Very Low Mars Orbit Atmosphere-Breathing Electric Propulsion Earth observation Space tug
isfreeaccess_bool	false
container_title	CEAS space journal
authorswithroles_txt_mv	Vaidya, S. @@aut@@ Traub, C. @@aut@@ Romano, F. @@aut@@ Herdrich, G. H. @@aut@@ Chan, Y.-A. @@aut@@ Fasoulas, S. @@aut@@ Roberts, P. C. E. @@aut@@ Crisp, N. H. @@aut@@ Edmondson, S. @@aut@@ Haigh, S. J. @@aut@@ Holmes, B. E. A. @@aut@@ Macario-Rojas, A. @@aut@@ Oiko, V. T. A. @@aut@@ Smith, K. L. @@aut@@ Sinpetru, L. A. @@aut@@ Becedas, J. @@aut@@ Sulliotti-Linner, V. @@aut@@ Christensen, S. @@aut@@ Hanessian, V. @@aut@@ Jensen, T. K. @@aut@@ Nielsen, J. @@aut@@ Bisgaard, M. @@aut@@ Garcia-Almiñana, D. @@aut@@ Rodriguez-Donaire, S. @@aut@@ Suerda, M. @@aut@@ Garcia-Berenguer, M. @@aut@@ Kataria, D. @@aut@@ Villain, R. @@aut@@ Seminari, S. @@aut@@ Conte, A. @@aut@@ Belkouchi, B. @@aut@@
publishDateDaySort_date	2022-03-21T00:00:00Z
hierarchy_top_id	626054389
id	SPR048168106
language_de	englisch
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author	Vaidya, S.
spellingShingle	Vaidya, S. misc Very Low Earth Orbit misc Very Low Mars Orbit misc Atmosphere-Breathing Electric Propulsion misc Earth observation misc Space tug Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)
authorStr	Vaidya, S.
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topic_title	Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP) Very Low Earth Orbit (dpeaa)DE-He213 Very Low Mars Orbit (dpeaa)DE-He213 Atmosphere-Breathing Electric Propulsion (dpeaa)DE-He213 Earth observation (dpeaa)DE-He213 Space tug (dpeaa)DE-He213
topic	misc Very Low Earth Orbit misc Very Low Mars Orbit misc Atmosphere-Breathing Electric Propulsion misc Earth observation misc Space tug
topic_unstemmed	misc Very Low Earth Orbit misc Very Low Mars Orbit misc Atmosphere-Breathing Electric Propulsion misc Earth observation misc Space tug
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title	Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)
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title_full	Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)
author_sort	Vaidya, S.
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author_browse	Vaidya, S. Traub, C. Romano, F. Herdrich, G. H. Chan, Y.-A. Fasoulas, S. Roberts, P. C. E. Crisp, N. H. Edmondson, S. Haigh, S. J. Holmes, B. E. A. Macario-Rojas, A. Oiko, V. T. A. Smith, K. L. Sinpetru, L. A. Becedas, J. Sulliotti-Linner, V. Christensen, S. Hanessian, V. Jensen, T. K. Nielsen, J. Bisgaard, M. Garcia-Almiñana, D. Rodriguez-Donaire, S. Suerda, M. Garcia-Berenguer, M. Kataria, D. Villain, R. Seminari, S. Conte, A. Belkouchi, B.
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author-letter	Vaidya, S.
doi_str_mv	10.1007/s12567-022-00436-1
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title_sort	development and analysis of novel mission scenarios based on atmosphere-breathing electric propulsion (abep)
title_auth	Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)
abstract	Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022
abstractGer	Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022
abstract_unstemmed	Abstract Operating satellites in Very Low Earth Orbit (VLEO) benefit the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term operations at such low altitudes require propulsion systems to compensate for the large aerodynamic drag forces. When using conventional propulsion systems, the amount of storable propellant limits the maximum mission lifetime. The latter can be avoided by employing Atmosphere-Breathing Electric Propulsion (ABEP) system, which collects the residual atmospheric particles and uses them as propellant for an electric thruster. Thus, the requirement of on-board propellant storage can ideally be nullified. At the Institute of Space Systems (IRS) of the University of Stuttgart, an intake, and a RF Helicon-based Plasma Thruster (IPT) for ABEP system are developed within the Horizons 2020 funded DISCOVERER project. To assess possible future use cases, this paper proposes and analyzes several novel ABEP-based mission scenarios. Beginning with technology demonstration mission in VLEO, more complex mission scenarios are derived and discussed in detail. These include, amongst others, orbit maintenance around Mars as well as refuelling and space tug missions. The results show that the ABEP system is not only able to compensate drag for orbit maintenance but also capable of performing orbital maneuvers and collect propellant for applications such as Space Tug and Refuelling. Thus, showing a multitude of different future mission applications. © The Author(s), under exclusive licence to Council of European Aerospace Societies 2022
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container_issue	4
title_short	Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)
url	https://dx.doi.org/10.1007/s12567-022-00436-1
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author2	Traub, C. Romano, F. Herdrich, G. H. Chan, Y.-A. Fasoulas, S. Roberts, P. C. E. Crisp, N. H. Edmondson, S. Haigh, S. J. Holmes, B. E. A. Macario-Rojas, A. Oiko, V. T. A. Smith, K. L. Sinpetru, L. A. Becedas, J. Sulliotti-Linner, V. Christensen, S. Hanessian, V. Jensen, T. K. Nielsen, J. Bisgaard, M. Garcia-Almiñana, D. Rodriguez-Donaire, S. Suerda, M. Garcia-Berenguer, M. Kataria, D. Villain, R. Seminari, S. Conte, A. Belkouchi, B.
author2Str	Traub, C. Romano, F. Herdrich, G. H. Chan, Y.-A. Fasoulas, S. Roberts, P. C. E. Crisp, N. H. Edmondson, S. Haigh, S. J. Holmes, B. E. A. Macario-Rojas, A. Oiko, V. T. A. Smith, K. L. Sinpetru, L. A. Becedas, J. Sulliotti-Linner, V. Christensen, S. Hanessian, V. Jensen, T. K. Nielsen, J. Bisgaard, M. Garcia-Almiñana, D. Rodriguez-Donaire, S. Suerda, M. Garcia-Berenguer, M. Kataria, D. Villain, R. Seminari, S. Conte, A. Belkouchi, B.
ppnlink	626054389
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hochschulschrift_bool	false
doi_str	10.1007/s12567-022-00436-1
up_date	2024-07-03T17:28:17.461Z
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Development and analysis of novel mission scenarios based on Atmosphere-Breathing Electric Propulsion (ABEP)

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