Communications Systems An/wsc-3 Parts

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Filter By: Diode Semiconductor Devices
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Part Number
NSN
NIIN
013-J5615 Diode Semiconductor Device
004269613
0196046P017 Diode Semiconductor Device
007526115
0403850002 Diode Semiconductor Device
004600981
1+4M2+4A25 Diode Semiconductor Device
009394263
1-4M2-4AZ Diode Semiconductor Device
011263009
100412 Diode Semiconductor Device
007526115
10133046 Diode Semiconductor Device
001724970
10133075 Diode Semiconductor Device
004072445
10133081 Diode Semiconductor Device
004269613
10133165 Diode Semiconductor Device
010439178
10133275 Diode Semiconductor Device
011263009
10388919 Diode Semiconductor Device
010679799
1080H80H17 Diode Semiconductor Device
005292685
1081H34H12 Diode Semiconductor Device
005292685
11-01938-00 Diode Semiconductor Device
009394263
11-09988-00 Diode Semiconductor Device
007526115
11-11577-00 Diode Semiconductor Device
010439178
110-328-22 Diode Semiconductor Device
004072445
110-328-29 Diode Semiconductor Device
004072445
12043-0075 Diode Semiconductor Device
007526115
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Communications Systems An/wsc-3

Picture of Communications Systems An/wsc-3

Space Network (SN) is a NASA program that combines space and ground elements to support spacecraft communications in Earth vicinity. The SN Project Office at Goddard Space Flight Center (GSFC) manages the SN, which consists of:

Tracking and Data Relay Satellite (TDRS) currently consists of first generation (F1-F7), and second generation (F8-F10) satellites.

The space segment of the SN consists of up to six operational relay satellites in geosynchronous orbit. These communications satellites are allocated longitudes for relaying forward and return service signals to and from customers, any entity with an Earth-orbiting satellite that has an agreement with SN to use its communications services, for data transfer and tracking. An additional TDRS, F1, provides dedicated support to the National Science Foundation (NSF) through the use of the WSC Alternate Relay Terminal (WART). Additional spare TDRSs may be in geosynchronous orbit.

All first generation TDRSs (F1-F7, also known as TDRS A-G) carry functionally identical payloads and all second generation TDRSs (F8-F10, also known as TDRS H-J) carry functionally identical payloads.

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