Project Overview

SRLSAT team is a student team composed of university staff, Ph.D., M.Sc., and B.Sc students from Aerospace, Electrical, and Computer Engineering faculties under the supervision of the SRL technical team. SRLSAT is a 6U CubeSat with a Communication mission. The project is completed the conceptual design phase and is now in the preliminary design phase. SRLSAT will have an orbit with 500 km altitude, a 98-degree inclination, and 1 year lifetime. The team is designing all subsystems, including ADCS, EPS, C&DH, TT&C, TC, STR, and mechanisms. In the next step, they will go through a detailed design phase and engineering model.


SRLSAT team contains different specialists in Aerospace engineering, Space system engineering, Electrical, telecommunications.


System and Subsystem Properties



Contact Info

Space Research Laboratory, Aerospace Engineering Faculty, K. N. Toosi University of Technology, Daneshgah Blvd., Ehsan Exit, East Zeynoddin Highway, Tehran, Iran

Phone: +98 21 77334133

Fax: +98 21 73064234

Web: Spacerl

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