The novel design and development of Inter Satellite link subsystem for Low Earth Orbit Satellites.
- Paper number
IAC-23,B2,5,2,x79804
- Author
Dr. Somaia Mohamed, Egyptian Space Agency (EgSA), Egypt
- Coauthor
Dr. Haitham Akah, National Authority for Remote Sensing and Space Sciences (NARSS), Egypt
- Coauthor
Mrs. Ranya Salah Elagooz, Egyptian Space Agency (EgSA), Egypt
- Coauthor
Mrs. Thoria Afifi, Egyptian Space Agency (EgSA), Egypt
- Coauthor
Ms. Hoda Elmegharbel, Egyptian Space Agency (EgSA), Egypt
- Year
2023
- Abstract
The Satellite constellations have a special capability to provide unique and new applications such as cellular telephone networks, stable and high-speed internet over satellite, etc. The satellite constellation in the LEO orbit will provide many services at a reduced cost. So, the inter-satellite link is a vital subsystem in the satellite constellation. The Inter-satellite link (ISL) Transceiver is the core of the satellite platform in the satellite constellation, which is one of the most important subsystems in satellites. It is the link between the satellite, the Ground control station, and other satellites in the constellation, as well as working as a hub between the satellites. This paper will demonstrate the mission analysis of the constellation that determined the requirements of the ISL subsystem and all phases of design and development of the subsystem. The ISL subsystem operates in the S-band frequency, with a data rate up to 100kbp and RF output power of 1watt, using the CCSDS protocol.
- Abstract document
- Manuscript document
IAC-23,B2,5,2,x79804.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.