Abstract “Tian Tuo 1”(TT-1) nano-satellite is the first single-board nano-satellite that was
successfully launched in China. The main objective of TT-1 is technology demonstration and …

Over 400 CubeSats have been launched during the first 13 years of existence of this 10 cm
cube-per unit standard. The CubeSat's flexibility to use commercial-off-the-shelf (COTS) …

A new method for measuring the performance of a micro-thruster is suggested in this paper.
A few thrust stands have been developed for measuring micro-level thrusts. This paper …

This paper presents the development of a new approach for the Payload Control and Data
Acquisition Subsystem (PCDAS) to be applied in micro-, up to small-satellite systems in low …

This paper presents a template architecture for a straightforward specification of small
satellite missions by means of a domain specific language. Furthermore, the process to …

This thesis presents a qualitative and quantitative comparison between an MMIC LNA
packaged on PCB, and hybrid LNAs at V-band. This includes a quantitative study of the TID …

ABSTRACT The French South African Institute of Technology (F'SATI) at the Cape Peninsula
University of Technology (CPUT) began a program in Satellite Systems Engineering in 2009 …

This chapter introduces the main real‐time operational system (RTOS) concepts and the
current state of their use in nanosatellite missions—pointing out their successes and failures …

A new method for measuring performance of a micro-thruster is suggested in this paper. A
few thrust stands have been developed for measuring micro-level thrusts. This paper …

This paper presents a comparison of two different system architectures, from receive
antenna to digitisation, for a compact, low cost mm-wave sun observation instrument. A …