1–17 of 17 hits
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    System modelling of very low Earth orbit satellites for Earth observation

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

    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

    The benefits of very low earth orbit for earth observation missions

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

    Attitude control for satellites flying in VLEO using aerodynamic surfaces

    Free access
    Munoz, VC / Gonzalez, D / Becedas, J et al. | BASE | 2020

    Structural design and test capability of a CFRP aileron

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

    Electromagnetic compatibility between 25kV - 50 Hz rail system and parallel 3 k V d.c. lines: influence on d.c. electronic traction converters

    Carillo, D. / Cavaliere, F. / Gaggelli, A. et al. | British Library Conference Proceedings | 2002

    Integration of time-domain simulation models for vehicles and components

    Romano, F. / Cau, G. / Fay, A. et al. | British Library Conference Proceedings | 2000

    User-friendly codes for heat transfer calculations

    Torella, G. / Romano, F. / Manca, O. | AIAA | 1998

    La Marina Militare attraverso il francobollo postale

    Romano, F. | Online Contents | 1996