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Abstract
The Satellite for Orbital Aerodynamics Research (SOAR) is a 3U CubeSat that has been designed to investigate the aerodynamic performance of different materials at low orbital altitudes. The spacecraft has been developed within the scope of DISCOVERER, a Horizon 2020 project that aims to develop foundational technologies to enable
sustainable operations of Earth observation spacecraft in very low Earth orbits (VLEO) i.e., those below 450 km.
SOAR features two payloads: i) a set of steerable fins that can expose different materials to the oncoming atmospheric flow developed by The University of Manchester, and ii) a forward-facing ion and neutral mass spectrometer (INMS)
that provides in-situ measurements of the atmospheric density, flow composition, and velocity from the Mullard Space Science Laboratory (MSSL) of University College London. These payloads enable characterisation of the aerodynamic performance of different materials at very low altitudes with the aim to advance understanding of the underlying gassurface interactions in rarefied flow environments. The satellite will also be used to test novel aerodynamic attitude control methods and perform atmospheric characterisation in the VLEO altitude range. SOAR will perform the first in-orbit test of two novel materials that are expected to have atomic oxygen erosion resistance and drag-reducing properties, providing valuable in-orbit validation data for ongoing ground-based experimentation. Such materials hold the promise for extending operations at lower altitudes with benefits particularly for Earth observation and
communications satellites that can correspondingly be reduced in size and cost. The platform for SOAR is largely based on GOMX-3 heritage and the spacecraft was assembled, integrated, and tested by GomSpace A/S. The satellite was launched on the SpX-22 commercial resupply service mission to the International Space Station in on 3rd June 2021 was subsequently deployed into orbit on the 14th June 2021. This paper presents the final preparations of SOAR prior to launch and provides an overview of the planned operations of the spacecraft following deployment into orbit.
Keywords: Orbital Aerodynamics; Drag and Lift Coefficient; Gas-Surface Interactions; Thermospheric Wind; CubeSat.
sustainable operations of Earth observation spacecraft in very low Earth orbits (VLEO) i.e., those below 450 km.
SOAR features two payloads: i) a set of steerable fins that can expose different materials to the oncoming atmospheric flow developed by The University of Manchester, and ii) a forward-facing ion and neutral mass spectrometer (INMS)
that provides in-situ measurements of the atmospheric density, flow composition, and velocity from the Mullard Space Science Laboratory (MSSL) of University College London. These payloads enable characterisation of the aerodynamic performance of different materials at very low altitudes with the aim to advance understanding of the underlying gassurface interactions in rarefied flow environments. The satellite will also be used to test novel aerodynamic attitude control methods and perform atmospheric characterisation in the VLEO altitude range. SOAR will perform the first in-orbit test of two novel materials that are expected to have atomic oxygen erosion resistance and drag-reducing properties, providing valuable in-orbit validation data for ongoing ground-based experimentation. Such materials hold the promise for extending operations at lower altitudes with benefits particularly for Earth observation and
communications satellites that can correspondingly be reduced in size and cost. The platform for SOAR is largely based on GOMX-3 heritage and the spacecraft was assembled, integrated, and tested by GomSpace A/S. The satellite was launched on the SpX-22 commercial resupply service mission to the International Space Station in on 3rd June 2021 was subsequently deployed into orbit on the 14th June 2021. This paper presents the final preparations of SOAR prior to launch and provides an overview of the planned operations of the spacecraft following deployment into orbit.
Keywords: Orbital Aerodynamics; Drag and Lift Coefficient; Gas-Surface Interactions; Thermospheric Wind; CubeSat.
| Original language | English |
|---|---|
| Title of host publication | 72nd International Astronautical Congress |
| Publication status | Accepted/In press - 25 Oct 2021 |
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Space Systems Research Group
Smith, K. (PI), Roberts, P. (PI), Crisp, N. (PI), Mcgrath, C. (PI), Parslew, B. (CoI), Hollingsworth, P. (CoI), Utyuzhnikov, S. (CoI), Lo, K. C. J. (Researcher), Muirhead, I. (PGR student), Wijacinski, K. (PGR student), Kent, B. (PGR student), Mackintosh, J. (PGR student) & Lopez Pardo, B. (PGR student)
Project: Research
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DISCOVERER: Disruptive Technologies for Very Low Earth Orbit Platforms
Roberts, P. (PI), Edmondson, S. (CoI), Haigh, S. (CoI), Smith, K. (CoI) & Crisp, N. (Researcher)
1/01/17 → 31/03/22
Project: Research
Impacts
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Very Low Earth Orbits (VLEO) satellites - impacts from the DISCOVERER project
Roberts, P. (Participant), Smith, K. (Participant), Crisp, N. (Participant), Edmondson, S. (Participant) & Haigh, S. (Participant)
Impact: Economic, Technological, Policy