activity
20202024
most citedThe Benefits of Very Low Earth Orbit for Earth Observation Missions

253 citations · 628 across the 9 of their papers we have counts for

collaborators

9 papers

physics.space-ph2024

Performance Test Methodology for Atmosphere-Breathing Electric Propulsion Intakes in an Atomic Oxygen Facility

Alexander T. Cushen, Vitor T. A. Oiko, Katharine L. Smith +5

The testing of atmosphere-breathing electric propulsion intakes is an important step in the development of functional propulsion systems which provide sustained drag compensation i…

physics.space-ph2022★ 20 cited

Design of an Intake and a Thruster for an Atmosphere-Breathing Electric Propulsion System

F. Romano, G. Herdrich, Y. -A. Chan +25

Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft that finally defines the missions lifetime unle…

physics.space-ph2022★ 27 cited

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

S. Vaidya, C. Traub, F. Romano +28

Operating satellites in Very Low Earth Orbit (VLEO) benefits the already expanding New Space industry in applications including Earth Observation and beyond. However, long-term ope…

physics.space-ph2022★ 11 cited

Uncertainties and Design of Active Aerodynamic Attitude Control in Very Low Earth Orbit

Sabrina Livadiotti, Nicholas H. Crisp, Peter C. E. Roberts +4

This paper discusses the design and the performance achievable with active aerodynamic attitude control in very low Earth orbit, i.e. below 450 km in altitude. A novel real-time al…

physics.space-ph2021★ 79 cited

System Modelling of Very Low Earth Orbit Satellites for Earth Observation

N. H. Crisp, P. C. E. Roberts, K. L. Smith +7

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. Critically, for Earth observ…

physics.space-ph2021★ 90 cited

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

F. Romano, J. Espinosa-Orozco, M. Pfeiffer +29

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 ef…

physics.space-ph2020★ 57 cited

In-Orbit Aerodynamic Coefficient Measurements using SOAR (Satellite for Orbital Aerodynamics Research)

N. H. Crisp, P. C. E. Roberts, S. Livadiotti +26

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

physics.space-ph2020★ 91 cited

A Review of Gas-Surface Interaction Models for Orbital Aerodynamics Applications

Sabrina Livadiotti, Nicholas H. Crisp, Peter C. E. Roberts +29

Renewed interest in Very Low Earth Orbits (VLEO) - i.e. altitudes below 450 km - has led to an increased demand for accurate environment characterisation and aerodynamic force pred…

physics.space-ph2020★ 253 cited

The Benefits of Very Low Earth Orbit for Earth Observation Missions

N. H. Crisp, P. C. E. Roberts, S. Livadiotti +30

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 tha…