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MISSION ANALYSIS OF A NEW SOLAR SAIL SATELLITE CONCEPT AT LOW EARTH ORBIT
Date
2021-01-01
Author
Polat, Hakkı
Tekinalp, Ozan
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© 2021, Univelt Inc. All rights reserved.Exploiting the propellant free maneuver capability of solar sail satellites for high resolution Earth observation mission is addressed with an elliptical low Earth orbit. The employed orbit has a low perigee altitude for observation and a high apogee altitude for orbit maneuvers. For the purpose of mission analysis of this new concept, a reference satellite configuration is designed with an aim to determine the technological readiness level based on the characteristic acceleration. Finally, a mission orbit parameter selection algorithm for a region of interest is developed based on observation performance metrics. The new concept is shown to be successful in carrying out propellant-free Earth observation.
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85126234730&origin=inward
https://hdl.handle.net/11511/98913
Conference Name
AAS/AIAA Astrodynamics Specialist Conference, 2020
Collections
Department of Aerospace Engineering, Conference / Seminar
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H. Polat and O. Tekinalp, “MISSION ANALYSIS OF A NEW SOLAR SAIL SATELLITE CONCEPT AT LOW EARTH ORBIT,” Virtual, Online, 2021, vol. 175, Accessed: 00, 2022. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85126234730&origin=inward.
