SERVIS 1
Japan
Spacecraft n°:
Japanese spacecraft n°: 115
Space Environment Reliability Verification Integrated System
Launch data:
Designation
28060 / 03050A
Launch date
30 Oct 2003 - 13:43:42 UT
Launch site
Plesetsk, LC133/3
Launch vehicle
Rokot/Briz-KM1 (#10)
Mission
Commercial: Technology development
Sun-Synchronous LEO Earth orbit:
Perigee/Apogee
984 x 1015 km
Eccentricity
2,10E-03
Inclination
99.5°
Period
105.1 min
Will evaluate COTS components in space environment and a lithium-ion battery.
Specifications:
Prime contractor
Institute for Unmanned Space Experiment Free Flyer (USEF)
Platform
Operator
Institute for Unmanned Space Experiment Free Flyer (USEF)
Mass at launch
980 kg
Mass in orbit
850 kg
Dimension
1.4 x 1.4 x 2.3 m
Solar array
Stabilization
DC power
EOL: 1200 W
Design lifetime
2 yrs
Decay:
Out of service:
July 2010
Cause:
no more active
Descent date:
Lifetime:
Mission details:
Utilization of commercial off-the-shelf components in space conditions
Ref: #7, #15, #226, #245 - update: 19.08.10