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Micro-Sat Structural Design and Development for a Very High-Resolution Earth Observation Payload

  • Bilge Memis*
  • , Onur Oztekin
  • , Alim Rustem Aslan
  • *Bu çalışma için yazışmadan sorumlu yazar
  • Istanbul Technical University

Araştırma çıktısı: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › Hakemli

Özet

Micro-Sats under 50 kg mass now reached the capability to host high performance payloads for a number of missions. Majority of missions are communications and earth observation. Present work is for a 1.5m/pixel GSD at 500km multispectral payload. High performance observation missions require tight compliance with payload operational requirements leading to micrometer tolerances both in mechanical design and manufacturing. The present paper details payload requirements relations to design and manufacturing with evaluations based on in orbit operations.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıRAST 2026 - 11th International Conference on Recent Advances in Air and Space Technologies, Conference Program
YayınlayanInstitute of Electrical and Electronics Engineers Inc.
ISBN (Elektronik)9798319546371
DOI'lar
Yayın durumuYayınlandı - 2026
Etkinlik11th International Conference on Recent Advances in Air and Space Technologies, Conference Program, RAST 2026 - Istanbul, Türkiye
Süre: 13 May 2026 → 15 May 2026

Yayın serisi

AdıRAST 2026 - 11th International Conference on Recent Advances in Air and Space Technologies, Conference Program

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???event.eventtypes.event.conference???11th International Conference on Recent Advances in Air and Space Technologies, Conference Program, RAST 2026
Ülke/BölgeTürkiye
ŞehirIstanbul
Periyot13/05/26 → 15/05/26

Bibliyografik not

Publisher Copyright:
© 2026 IEEE.

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