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 dil | İngilizce |
|---|---|
| Ana bilgisayar yayını başlığı | RAST 2026 - 11th International Conference on Recent Advances in Air and Space Technologies, Conference Program |
| Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
| ISBN (Elektronik) | 9798319546371 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2026 |
| Etkinlik | 11th 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
| Adı | RAST 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/Bölge | Türkiye |
| Şehir | Istanbul |
| Periyot | 13/05/26 → 15/05/26 |
Bibliyografik not
Publisher Copyright:© 2026 IEEE.
Parmak izi
Micro-Sat Structural Design and Development for a Very High-Resolution Earth Observation Payload' araştırma başlıklarına git. Birlikte benzersiz bir parmak izi oluştururlar.Alıntı Yap
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