[ARC5] ARC5 CW Question
w4thq at cox.net
w4thq at cox.net
Mon Jun 23 11:46:49 EDT 2014
The Apollo program during the 1960's and 1970's had complex relay logic in the control systems of both the launch vehicle and ground support equipment. Because of RFI-EMI problems, NASA required double-anode zeners across all 28 volt crystal-can relays. We found this approach was effective. We also discovered that the back-emf would "ring" and was not just one spike. The drop out time was not significant in our application so I don't remember what it was exactly.
John W4THQ
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