Sj. Gardner et al., THE DESIGN OF A SMALL SATELLITE FOR EARTH OBSERVATION, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 210(G4), 1996, pp. 323-332
The concept of the Teaching Company Scheme Satellite (TuCSAT), has bee
n developed to meet the requirements of the Earth observation user com
munity for inexpensive and flexible opportunities to launch remote sen
sing instruments into low earth orbit (LEG). This paper describes the
satellite design process, together with the philosophy behind the sele
ction of a baseline mission. The satellite is shown to demonstrate the
ability to meet a wide range of requirements within a strict low mass
and low cost philosophy, while making use of currently available tech
nology in order to achieve the design aims.