Experimental Results from the Satellite for Orbital Aerodynamics Research (SOAR) Mission

dc.contributor.authorCrisp, Nicholas H.
dc.contributor.authorMacario Rojas, Alejandro
dc.contributor.authorRoberts, Peter C.E
dc.contributor.authorGarcía-Almiñana, Daniel
dc.contributor.authorSureda Anfres, Miquel
dc.contributor.authorRodríguez Donaire, Silvia
dc.contributor.groupUniversitat Politècnica de Catalunya. TUAREG - Turbulence and Aerodynamics in Mechanical and Aerospace Engineering Research Group
dc.contributor.groupUniversitat Politècnica de Catalunya. L'AIRE - Laboratori Aeronàutic i Industrial de Recerca i Estudis
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria de Projectes i de la Construcció
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Física
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Organització d'Empreses
dc.date.accessioned2022-10-14T10:43:22Z
dc.date.issued2022
dc.description.abstractThe Satellite for Orbital Aerodynamics Research (SOAR) is a 3U CubeSat that has been designed to investigate the aerodynamic performance of different materials and perform demonstrations of aerodynamic attitude control manoeuvres in very low Earth orbit (VLEO). SOAR was deployed from the ISS on 14th June 2021 into a naturally decaying orbit and deorbited on 14th March 2022. This paper provides an overview of the operations performed during the mission and presents preliminary experimental results obtained from this spacecraft. SOAR was designed and launched within the frame of DISCOVERER, a Horizon 2020 project that aimed to support the development of a new class of commercially viable spacecraft operating in VLEO, i.e., orbits below 450 km in altitude. Operating in these lower altitude orbits has several benefits to the design of spacecraft, particularly for Earth observation and communications applications. However, development of spacecraft that can operate sustainably at these altitudes requires advancement in foundational technologies, for example atmosphere-breathing electric propulsion (ABEP) and novel aerodynamic materials. The primary aim of SOAR was to characterise the aerodynamic performance of different materials at very low altitudes and accomplished this task using a set of steerable fins that exposed different materials to the oncoming flow and an ion and neutral mass spectrometer (INMS) to provide in-situ measurements of atmospheric properties. SOAR was also designed to perform novel aerodynamic attitude control manoeuvres and measurements of thermospheric winds. Two of the materials carried to orbit were selected for their atomic oxygen erosion resistance and potential improvement in aerodynamic performance. The identification of such materials would allow for a reduction in the drag experienced in VLEO, the design of atmospheric intakes with greater efficiency used for ABEP, and implementation of enhanced aerodynamic attitude and orbit control. Ongoing ground-based experimentation seeks to further characterise the properties of such materials and to deepen our understanding of the physical interaction mechanisms that occur in the rarefied flow environment of VLEO.
dc.description.peerreviewedPeer Reviewed
dc.description.versionPostprint (published version)
dc.format.extent9 p.
dc.identifier.citationCrisp, N. [et al.]. Experimental Results from the Satellite for Orbital Aerodynamics Research (SOAR) Mission. A: International Astronautical Congress. "Proceedings of the 73rd International Astronautical Congress". International Astronautical Federation, 2022, p. 1-9. ISBN 0074-1795.
dc.identifier.isbn0074-1795
dc.identifier.urihttps://hdl.handle.net/2117/374439
dc.language.isoeng
dc.publisherInternational Astronautical Federation
dc.relation.projectidinfo:eu-repo/grantAgreement/EC/H2020/737183/EU/DISCOVERER – DISruptive teChnOlogies for VERy low Earth oRbit platforms/DISCOVERER
dc.relation.publisherversionhttps://iafastro.directory/iac/proceedings/IAC-22/
dc.rights.accessRestricted access - publisher's policy
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai::Astronàutica
dc.subjectÀrees temàtiques de la UPC::Enginyeria de la telecomunicació::Radiocomunicació i exploració electromagnètica::Satèl·lits i ràdioenllaços
dc.subject.lcshArtificial satellites -- Design and construction
dc.subject.lcshFlight control
dc.subject.lcshAerodynamics
dc.subject.lemacSatèl·lits artificials -- Disseny i construcció
dc.subject.lemacSistemes de control (Vol)
dc.subject.lemacAerodinàmica
dc.subject.otherOrbital Aerodynamics
dc.subject.otherDrag and Lift Coefficient
dc.subject.otherGas-Surface Interactions
dc.subject.otherCubeSat
dc.titleExperimental Results from the Satellite for Orbital Aerodynamics Research (SOAR) Mission
dc.typeConference report
dspace.entity.typePublication
local.citation.authorCrisp , N.; Macario, A.; Roberts, P.; Garcia-Almiñana, Daniel; Sureda, M.; Rodriguez-Donaire, S.
local.citation.contributorInternational Astronautical Congress
local.citation.endingPage9
local.citation.publicationNameProceedings of the 73rd International Astronautical Congress
local.citation.startingPage1
local.identifier.drac34246723

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