November 5,2007

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Gsat 14

 2014-001A

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I2K bus, Mass 1982 kg wet 851 kg dry. 2.0 x 2.0 x 3.6m, + 2 pan. The second flight of the GSLV with the indigenous CUS stage and cryo engine, and its first success, following D3 failure. Had a 3.4-m fairing instead of the 4-m fairing used on F06/D3. CUS is 8.7m long 2.8m dia and carries 12800 kg of LOX/LH2; engine is 73.55 kN and burns for 720s.

GSAT 14
Date	Time	Event	Orbit
2014 Jan 5	1048	Launch by GSLV Mk II D5	SDSC SLP
		T+2:29 SOM shutdown 71 km
		T+2:29 St 2 burn
		T+2:31 St 1 sep 72 km	-6072 x 81?
		T+3:46 PLF sep 115 km	-5706 x 114?
	1052	T+4:49 GS2 MECO 132 km
		T+4:52 GS2 sep
		T+4:53 CUS-12 ignition	-4753 x 133
	1104	T+16:55 CUS MECO 302 km
	1105	T+17:08 CUS sep 213 km	180 x 35975 x 19.3 (PK)
			630.13 160 x 35777 x 19.4
			630.15 182 x 35755 x 19.4
2014 Jan 6	0528s	LAM-1	807.84 8942 x 35766 x 7.6
2014 Jan 7	s	LAM-2
2014 Jan 7			1352.92 32543 x 35741 x 0.7 GEO 17.0E+22E/d
2014 Jan 9	s	LAM-3