SERVIS-2

 2010-023A

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Space Environment Reliability Verification Integrated System. SERVIS-2 will launch on Rokot from Plesetsk in 2010. Mass 740 kg. Orbit 1200 x 1200 x 100.42. Funded by Ministry of Economics, Trade and Industry (METI) and NEDO (New Energy and Industrial Technology Dev. Organization); operated by Institute for USEF, Tokyo. Project is to space-qualify commercial off-the-shelf parts for use on spacecraft.

Size 2.3 x 1.5m x 1.4m, 10.2m span.

SERVIS-2
Date	Time	Event	Orbit
2010 Jun 2	0159:12	Launch by Rokot	PL LC133/3
	0201:17	T+2:06 St 1 sep 68 km	-5911 x 158 x 99
	0201:20	St 2 burn
	0202:03	T+3:09 Fairing 121 km	-5705 x 184 x 99
	0204:19	St 2 MECO
	0204:20	T+5:19 St 2 sep 238 km 8 deg 5.656 km/s	-4058 x 309 x 99
	0204:26	T+5:25 Briz MES-1
		St 2 impact at 77 11 N 75 18W 3868 km range
	0213:18	T+13:47 MECO-1	153 x 1177 x 99.45
	0314:05	T+1:15:04 MES-2
	0314:50	T+1:15:48 MECO-2
	0336:30	T+1:37:30 Briz sep from SERVIS-2	1186 x 1210 x 100.4
	0346:31	T+1:47:30 Briz MES-3 lower orbit
	0349:11	T+1:50:10 Briz MECO-3	877 x 1206 x 100.6

Payload:

• CPTU Commercial Parts Test Unit (SRAM, DRAM, Flash Mem, FPGA)

• COTS COTS equipment

  • LIBA Li Ion (Mn type) Battery System with Automotive Technology

  • ADMS High Assurance Data Management System

  • CRAFT Fault Tolerant Computer with CRAFT system

  • PPRTU Plug and Play Remote Terminal Unit

  • HPDC High Performance Data Compressor

  • APE Advanced Positioning Experimental Module