1–12 von 12 Ergebnissen
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    The benefits of very low earth orbit for earth observation missions

    Crisp, N.H. / Roberts, P.C.E. / Livadiotti, S. et al. | Elsevier | 2020

    System modelling of very low Earth orbit satellites for Earth observation

    Crisp, N.H. / Roberts, P.C.E. / Romano, F. et al. | Elsevier | 2021

    Structural design and test capability of a CFRP aileron

    Romano, F. / Fiori, J. / Mercurio, U. | Tema Archiv | 2009

    La Marina Militare attraverso il francobollo postale

    Romano, F. | Online Contents | 1996

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

    Romano, F. / Espinosa-Orozco, J. / Pfeiffer, M. et al. | Elsevier | 2021

    In-orbit aerodynamic coefficient measurements using SOAR (Satellite for Orbital Aerodynamics Research)

    Crisp, N.H. / Roberts, P.C.E. / Livadiotti, S. et al. | Elsevier | 2020

    Influence of chemical models on the computation of thermo-fluid-dynamic parameters in hypersonic, rarefied flows

    Zuppardi, G / Morsa, L / Romano, F | SAGE Publications | 2010

    Attitude control for satellites flying in VLEO using aerodynamic surfaces

    Freier Zugriff
    Munoz, VC / Gonzalez, D / Becedas, J et al. | BASE | 2020