Since 1975, MECANEX S.A. has been manufacturing components for solar array drives and mechanisms used in space applications. In 1991, work was started in an early phase C (Engineering Model) on a Coarse Pointing Mechanism Assembly (CPMA) for the Semiconductor-laser Inter-satellite Link EXperiment (SILEX). This paper deals with the history, the evolution, and the lessons learned from taking over a pre-design in 1991 to the delivery of last flight models (FM 5 & 6) in 1995.
Coarse pointing mechanism assembly for satellite interlink experiment
01.05.1996
Aufsatz (Konferenz)
Keine Angabe
Englisch
Coarse Pointing Mechanism Assembly for Satellite Interlink
British Library Conference Proceedings | 1996
|Interlink and coverage analysis for small satellite constellations
Online Contents | 2013
|Interlink and coverage analysis for small satellite constellations
SAGE Publications | 2013
|A Coarse Pointing Assembly for Optical Communication
NTRS | 2010
|Contraves optical terminal-coarse pointing assembly (CPA)
British Library Conference Proceedings | 2003
|