Communications Systems An/wsc-3 Parts

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Filter By: Electrolytic Fixed Capacitors
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Part Number
NSN
NIIN
0180-0194 Electrolytic Fixed Capacitor
012600442
0180-1747 Electrolytic Fixed Capacitor
012600442
037-116 Electrolytic Fixed Capacitor
012600442
037-425 Electrolytic Fixed Capacitor
009593298
0905-101 Electrolytic Fixed Capacitor
012456442
1005572 Electrolytic Fixed Capacitor
012778529
10134947 Electrolytic Fixed Capacitor
011194298
10135068 Electrolytic Fixed Capacitor
012600442
10138665 Electrolytic Fixed Capacitor
011194348
10154292 Electrolytic Fixed Capacitor
012798138
10199-42472 Electrolytic Fixed Capacitor
009593298
102-361-002 Electrolytic Fixed Capacitor
011194305
10544805 Electrolytic Fixed Capacitor
011194348
109D167X0050W2 Electrolytic Fixed Capacitor
011194348
109D167X9050W2 Electrolytic Fixed Capacitor
011194348
109D277X9015T2 Electrolytic Fixed Capacitor
011194305
11-00374-013 Electrolytic Fixed Capacitor
010160110
11-00599-126 Electrolytic Fixed Capacitor
009593298
11065242-001 Electrolytic Fixed Capacitor
012501345
1111058-15 Electrolytic Fixed Capacitor
011194348
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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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