Impact of Noise Figure on a Satellite Link Performance

Small satellite link performance analysis is critical for assessing the adequacy of a transmitter to successfully transfer data at the desired rate. This is especially obvious when considering highly adaptive small satellite systems that exhibit static and active/dynamic power requirements. This paper presents the impact of noise figure on the carrier and data links performances of a highly adaptive small satellite application. The noise figures of a MMIC LNA, designed using GaAs technology operating within the C- and X-bands, were used to study the link performance of a planetary mission. An existing Magellan spacecraft link performance was considered in this study. The analysis reveals that designing a broadband LNA to have a ripple of less than 0.1 dB within its operating bandwidth is essential for a less than 2 dB drop in the carrier and data links margins. This fixes a 6.8 K receiver noise temperature swing margin for reliable, dynamic, broadband and adaptive space operations.

[1]  Tanya Vladimirova,et al.  Dual Core System-on-a-Chip Design to Support Inter-Satellite Communications , 2008, 2008 NASA/ESA Conference on Adaptive Hardware and Systems.

[2]  Danielle George,et al.  4 – 8 GHz LNA design for a highly adaptive small satellite transponder using InGaAs pHEMT technology , 2010, 2010 IEEE 11th Annual Wireless and Microwave Technology Conference (WAMICON).

[3]  Charles D. Brown Elements of Spacecraft Design , 2002 .

[4]  Martin Sweeting,et al.  Very-Small-Satellite Design for Distributed Space Missions , 2007 .

[5]  Danielle George,et al.  A system-based design methodology and architecture for highly adaptive small satellites , 2010, 2010 IEEE International Systems Conference.

[6]  Daniel E. Hastings,et al.  Spacecraft Design Lifetime , 2002 .

[7]  M. Wittig,et al.  Satellite onboard processing for multimedia applications , 2000, IEEE Commun. Mag..

[8]  B. Jackson,et al.  A reconfigurable multifunctional architecture approach for next-generation nanosatellite design , 2000, 2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484).

[9]  Zhenwei Hou,et al.  Flexible electronic assemblies for space applications , 2010, IEEE Aerospace and Electronic Systems Magazine.