2008-030B
Thales Alenia Space Spacebus 4000B2 with 24 Ku. Mass 3110 kg launch, 1272 kg dry (AriPK);
Size 2.8 x 1.8 x 2.9m, span 29.6m.
Delivery on orbit to Turksat AS via Ariane 5; will replace Turksat 1C.
Flight V183 with vehicle L540.
EAP type B, 31m high 3m dia with 38t empty mass and 240t of prop. EPC type C (H175/Vulcain 2) is 30m long 5.4m dia, 14100 kg dry. VEB type C and Cone 3936 is 950 kg; ESC-A is 19000 kg full. Astrium-ST SYLDA 5A is 400-530 kg 6.4m high 4.6m dia; ACU are 150 kg each, two EADS-CASA PAS 1194C. Long Fairing is 2000-2500 kg.
Performance margine is used to reduce inclination from 6 deg to 2 deg.
VEB/ESC-A/Cone 3936 are now produced in Astrium ST/Bremen. (This is the third one to be done in Bremen, to accommodate higher production rates.)
| Turksat 3A | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2008 Jun 12 | 2205:02 | Ignition | |
| 2205:09 | Launch | ||
| T+1:53 EAP sep | |||
| T+3:04 Fairing sep | |||
| T+8:49 EPC MECO | |||
| T+8:55 EPC sep | -1062 x 172 x 6.8 | ||
| T+8:59 ESC-A burn | |||
| T+24:45 ESC-A MECO | |||
| T+27:02 Skynet 5C sep | |||
| T+29:25 SYLDA sep | |||
| T+31:39 Turksat 3A sep | |||
| 2008 Jun 13 | 630.39 254 x 35696 x 2.0 | ||
| 2008 Jun 22 | 630.20 264 x 35677 x 2.0 | ||
| 2008 Jun 24 | LAM? | ||
| 2008 Jun 25 | 1436.09 35784 x 35788 x 0.1 GEO 31.0E | ||
| 2008 Jul 9 | mv out from 31E | ||
| 2008 Jul 17 | mv in at 42E | ||
| 2008 Aug 1 | 1436.08 35775 x 35796 x 0.0 GEO 42.0E | ||
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