Mutual Coupling of Internal Transmit/Receive Pair in Launch Vehicle Fairing Model Using WIPL-DEvaluating the fairing Radio Frequency (RF) Environment within the launch vehicle payload fairing cavity due to internal transmitters is an issue for the spacecraft and launch vehicle industry. This paper provides an effective approach for launch vehicle fairing evaluation of power reception and field distribution due to internal transmitters. A commercial electromagnetic computational tool, WIPL-D is applied in this study for test data comparison.
Document ID
20100042608
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Trout, Dawn H. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Stanley, James E. (Florida Inst. of Tech. Melbourne, FL, United States)
Wahid, Parveen F. (University of Central Florida Orlando, FL, United States)