RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)

Autor: Miquel Sureda, Badia Belkouchi, Valentín Cañas, Silvia Rodriguez-Donaire, C. Traub, Sabrina Livadiotti, R. M. Dominguez, Steve Edmondson, Jonathan Becedas, Francesco Romano, Alastair Straker, Peter Roberts, Rachel Villain, Sarah J. Haigh, V. Sulliotti-Linner, R. Outlaw, Daniel García-Almiñana, V. Hanessian, Morten Bisgaard, A. Conte, Yung-An Chan, A. Mølgaard, Jens Nielsen, Luciana Sinpetru, Stefanos Fasoulas, David Gonzalez, Nicholas Crisp, Dhiren Kataria, B. Heißerer, Georg H. Herdrich, A. Schwalber, Stephen D. Worrall, Claire Huyton, Vitor Toshiyuki Abrao Oiko, J. S. Perez, Katharine Smith

Publikováno v: Romano, F, Chan, Y, Herdrich, G, Traub, C, Fasoulas, S, Roberts, P, Smith, K, Edmondson, S, Haigh, S, Crisp, N, Oiko, V T A, Worrall, S D, Livadiotti, S, Huyton, C, Sinpetru, L, Straker, A, Becedas, J, Domínguez, R M, González, D, Cañas, V, Sulliotti-linner, V, Hanessian, V, Mølgaard, A, Nielsen, J, Bisgaard, M, Garcia-almiñana, D, Rodriguez-donaire, S, Sureda, M, Kataria, D, Outlaw, R, Villain, R, Perez, J S, Conte, A, Belkouchi, B, Schwalber, A & Heißerer, B 2020, ' RF helicon-based inductive plasma thruster (IPT) design for an Atmosphere-Breathing Electric Propulsion system (ABEP) ', Acta Astronautica . https://doi.org/10.1016/j.actaastro.2020.07.008
Acta Astronautica
UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)

Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamicdrag on the spacecraft. To extend such missions lifetime, an efficient propulsion system is required. Onesolution is Atmosphere-Breathing Ele

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d854bc8ffc2e0f3f811d43429bbc6cb5
https://doi.org/10.1016/j.actaastro.2020.07.008

The Benefits of Very Low Earth Orbit for Earth Observation Missions

Autor: R. M. Dominguez, Dhiren Kataria, Claire Huyton, Rachel Villain, Miquel Sureda, Katherine Smith, Silvia Rodriguez-Donaire, Francesco Romano, Jens Frederik Dalsgaard Nielsen, Sarah J. Haigh, Yung-An Chan, Nicholas Crisp, V. Hanessian, Stephen D. Worrall, C. Traub, Sabrina Livadiotti, Daniel García-Almiñana, Georg H. Herdrich, David Gonzalez, Morten Bisgaard, A. Conte, Steve Edmondson, Stefanos Fasoulas, Vitor Toshiyuki Abrao Oiko, B. Heißerer, J. S. Perez, A. Mølgaard, Badia Belkouchi, Peter Roberts, Luciana Sinpetru, Jonathan Becedas, R. Outlaw, A. Schwalber

Publikováno v: Crisp, N, Roberts, P, Livadiotti, S, Abrao Oiko, V T, Edmondson, S, Haigh, S, Huyton, C, Sinpetru, L, Smith, K, Worrall, S, Becedas, J, Dominiguez, R M, Gonzalez, D, Hanessian, V, Molgaard, A, Nielsen, J, Bisgaard, M, Chan, Y A, Fasoulas, S, Herdrich, G H, Romano, F, Traub, C, Garcia-Alminana, D, Rodriguez-Donaire, S, Sureda, M, Kataria, D, Outlaw, R, Belkouchi, B, Conte, A, Perez, J S, Villain, R, Heiberer, A & Schwalber, A 2020, ' The Benefits of Very Low Earth Orbit for Earth Observation Missions ', Progress in Aerospace Sciences, vol. 117 . https://doi.org/10.1016/j.paerosci.2020.100619
UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)
Progress in Aerospace Sciences

Very low Earth orbits (VLEO), typically classified as orbits below approximately 450 km in altitude, have the potential to provide significant benefits to spacecraft over those that operate in higher altitude orbits. This paper provides a comprehensi

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::28d35d1fe8513c683b35cce4416d7182
https://www.research.manchester.ac.uk/portal/en/publications/the-benefits-of-very-low-earth-orbit-for-earth-observation-missions(4fc18317-c19b-4316-a660-ad6899d72fbf).html

On the exploitation of differential aerodynamic lift and drag as a means to control satellite formation flight

Autor: Steve Edmondson, Leonardo Ghizoni, Gerardo González, Stephen D. Worrall, Peter Roberts, Sarah J. Haigh, Sabrina Livadiotti, R. M. Dominguez, R. Outlaw, Daniel García-Almiñana, Badia Belkouchi, Rachel Villain, Francesco Romano, Nicholas Crisp, Vitor Toshiyuki Abrao Oiko, Stefanos Fasoulas, J. S. Perez, Adam Boxberger, B. Heißerer, Miquel Sureda, Victor Jungnell, Silvia Rodriguez-Donaire, Kristian Bay, A. Conte, Jonathan Becedas, Rachel Lyons, Georg H. Herdrich, Jonas Morsbøl, Katharine Smith, A. Schwalber, Dhiren Kataria, T. Binder, David Gonzalez, C. Traub

Publikováno v: Traub, C, Romano, F, Binder, T, Boxberger, A, Herdrich, G H, Fasoulas, S, Roberts, P, Smith, K, Edmondson, S, Haigh, S, Crisp, N, Abrao Oiko, V T, Lyons, R, Worrall, S, Livadiotti, S, Becedas, J, Gonzalez, G, Dominguez, R M, Gonzalez, D, Ghizoni, L, Jungnell, V, Bay, K, Morsbøl, J, Garcia-Almiñana, D, Rodriguez-Donaire, S, Sureda, M, Kataria, D, Outlaw, R, Villain, R, Perez, J S, Conte, A, Belkouchi, B, Schwalber, A & Heißerer, B 2019, ' On the exploitation of differential aerodynamic lift and drag as a means to control satellite formation flight ', CEAS Space Journal, vol. 12 . https://doi.org/10.1007/s12567-019-00254-y
Recercat. Dipósit de la Recerca de Catalunya
instname
UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)
CEAS Space Journal

In order for a satellite formation to maintain its intended design despite present perturbations (formation keeping), to change the formation design (reconfiguration) or to perform a rendezvous maneuver, control forces need to be generated. To do so,

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::254b76f2820cd36ea156f1c5ffc23d8a
https://www.research.manchester.ac.uk/portal/en/publications/on-the-exploitation-of-differential-aerodynamic-lift-and-drag-as-a-means-to-control-satellite-formation-flight(218bf171-9d1f-46cf-b55d-b8cab8063476).html

Intake design for an Atmosphere-Breathing Electric Propulsion System (ABEP)

Autor: V. Hanessian, Brandon Holmes, Francesco Romano, Jens Nielsen, C. Traub, Jonathan Becedas, A. Macario-Rojas, Nicholas Crisp, Dhiren Kataria, Steve Edmondson, Rachel Villain, A. Conte, Luciana Sinpetru, Peter Roberts, J. Espinosa-Orozco, M. Pfeiffer, Simon Seminari, Simon Christensen, Badia Belkouchi, Vitor Toshiyuki Abrao Oiko, Yung-An Chan, Morten Bisgaard, T. Kauffman Jensen, Sarah J. Haigh, Miquel Sureda, Daniel García-Almiñana, Silvia Rodriguez-Donaire, V. Sulliotti-Linner, Sabrina Livadiotti, Stefanos Fasoulas, Katharine Smith, Georg H. Herdrich

Publikováno v: Romano, F, Espinosa-orozco, J, Pfeiffer, M, Herdrich, G, Crisp, N H, Roberts, P, Holmes, B E A, Edmondson, S, Haigh, S, Livadiotti, S, Macario-rojas, A, Oiko, V T A, Sinpetru, L A, Smith, K, Becedas, J, Sulliotti-linner, V, Bisgaard, M, Christensen, S, Hanessian, V, Jensen, T K, Nielsen, J, Chan, Y, Fasoulas, S, Traub, C, García-almiñana, D, Rodríguez-donaire, S, Sureda, M, Kataria, D, Belkouchi, B, Conte, A, Seminari, S & Villain, R 2021, ' Intake design for an Atmosphere-Breathing Electric Propulsion system (ABEP) ', Acta Astronautica . https://doi.org/10.1016/j.actaastro.2021.06.033
Acta Astronautica
UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)

Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft. To extend the lifetime of such missions, an efficient propulsion system is required. One solution is Atmosphere-Brea

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::36c088f835b12bec3691fa33f48f5c08