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Electronic timer for sounding rocket payload useAn electronic timer has been developed for sounding rocket use. The timer uses CMOS technology for low power consumption and has a battery back-up to keep the timing circuit active in case of a dropout on the payload power bus. Time-event decoding is done by programming EPROM's which enable a +28 volt dc sourcing output. There are 32 discrete outputs which can provide +28 volt dc into a minimum load impedance of 150 ohms. Inputs are designed to operate on standard CMOS voltage levels, but they can withstand +28 volts dc without damage. The timer can be started by either 'G' or lift-off switch closure or umbilical release at lift-off.
Document ID
19870028451
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, C. P.
(NASA Wallops Flight Center Wallops Island, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 86-2550
Accession Number
87A15725
Distribution Limits
Public
Copyright
Other

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