... 37 Chapter 5: Using multiple Matrox Pulsar boards . ... 72 Board input and output connectors . ... 88 Appendix C: Glossary Index A acceleration features, desktop 36 ActiveMIL-Lite 10, 14 analog cameras, attaching 23 analog input section 49, 69 analog switches, m onitor 62 analog-to-digital converters 50 digital video input 21 video input 21, 76 video output 2122, 75 conventions, manual 14 converters, analog-to-digital 50 D data interface section 55 DB-15 to 5-BNC cable 22 DB ...
... One can find basic technical characteristics of the SRT on the mission website.1 Originally, the launch of SRT of the RadioAstron mission was planned on 1994, and an orbit with the following initial parameters was selected: Perigee height , km Apogee height , km Inclination, deg Perigee argument, deg Longitude of ascending node, deg Period of revolution, h 4000 768000 51.5 300.0 190.0 28 The selection of an orbit with the above This orbit has a rather weak evolution. ...
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