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.

Team

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

Mission

System and Subsystem Properties

Achievements

2021-07-18T05:39:20+00:00

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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