Search Results - "Oiko, V.T.A."

The benefits of very low earth orbit for earth observation missions by Crisp, N.H., Roberts, P.C.E., Livadiotti, S., Oiko, V.T.A., Edmondson, S., Haigh, S.J., Huyton, C., Sinpetru, L.A., Smith, K.L., Worrall, S.D., Becedas, J., Domínguez, R.M., González, D., Hanessian, V., Mølgaard, A., Nielsen, J., Bisgaard, M., Chan, Y.-A., Fasoulas, S., Herdrich, G.H., Romano, F., Traub, C., García-Almiñana, D., Rodríguez-Donaire, S., Sureda, M., Kataria, D., Outlaw, R., Belkouchi, B., Conte, A., Perez, J.S., Villain, R., Heißerer, B., Schwalber, A.

“…Very low Earth orbits (VLEO), typically classified as orbits below approximately 450 km in altitude, have the potential to provide significant benefits to…”
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System modelling of very low Earth orbit satellites for Earth observation by Crisp, N.H., Roberts, P.C.E., Romano, F., Smith, K.L., Oiko, V.T.A., Sulliotti-Linner, V., Hanessian, V., Herdrich, G.H., García-Almiñana, D., Kataria, D., Seminari, S.

“…The operation of satellites in very low Earth orbit (VLEO) has been linked to a variety of benefits to both the spacecraft platform and mission design…”
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RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP) by Romano, F., Chan, Y.-A., Herdrich, G., Traub, C., Fasoulas, S., Roberts, P.C.E., Smith, K., Edmondson, S., Haigh, S., Crisp, N.H., Oiko, V.T.A., Worrall, S.D., Livadiotti, S., Huyton, C., Sinpetru, L.A., 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.

“…Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft. To extend such missions…”
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Intake design for an Atmosphere-Breathing Electric Propulsion System (ABEP) by Romano, F., Espinosa-Orozco, J., Pfeiffer, M., Herdrich, G., Crisp, N.H., Roberts, P.C.E., 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. Kauffman, Nielsen, J., Chan, Y.-A., Fasoulas, S., Traub, C., García-Almiñana, D., Rodríguez-Donaire, S., Sureda, M., Kataria, D., Belkouchi, B., Conte, A., Seminari, S., Villain, R.

“…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…”
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In-orbit aerodynamic coefficient measurements using SOAR (Satellite for Orbital Aerodynamics Research) by Crisp, N.H., Roberts, P.C.E., Livadiotti, S., Macario Rojas, A., Oiko, V.T.A., Edmondson, S., Haigh, S.J., Holmes, B.E.A., Sinpetru, L.A., Smith, K.L., Becedas, J., Domínguez, R.M., Sulliotti-Linner, V., Christensen, S., Nielsen, J., Bisgaard, M., Chan, Y.-A., Fasoulas, S., Herdrich, G.H., Romano, F., Traub, C., García-Almiñana, D., Rodríguez-Donaire, S., Sureda, M., Kataria, D., Belkouchi, B., Conte, A., Seminari, S., Villain, R.

“…The Satellite for Orbital Aerodynamics Research (SOAR) is a CubeSat mission, due to be launched in 2021, to investigate the interaction between different…”
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