This paper describes a system engineering approach to examining the potential for combining elements of a deep-space RF and optical communications payload, for the purpose of reducing the size, weight and power burden on the spacecraft and the mission. Figures of merit and analytical methodologies are discussed to conduct trade studies, and several potential technology integration strategies are presented. Finally, the NASA Integrated Radio and Optical Communications (iROC) project is described, which directly addresses the combined RF and optical approach.
Concurrent System Engineering and Risk Reduction for Dual-Band (RF/optical) Spacecraft Communications
2012
16 pages
Report
Keine Angabe
Englisch
Concurrent Engineering: Spacecraft and Mission Operations System Design
British Library Conference Proceedings | 1994
|