SERVIS

SERVIS 2

Japan

Spacecraft nº:

Japanese spacecraft nº: 166

SERVIS = Space Environment Reliability Verification Integrated System

Launch data:

Designation	36588 / 10023A
Launch date	02 Jun 2010 - 01:59 UT
Launch site	Plesetsk, LC-133/3
Launch vehicle	Rokot-KM
Mission	Commercial: Technology Development
Sun-Synchronous LEO Earth orbit on Jun 2.14:
Perigee / Apogee	1183 x 1211 km
Eccentricity	1.92E-03
Inclination	100.45 deg polar orbit
Period	109.37 min

Spacecraft data:

Prime contractor	Mitsubishi Electric (USEF?)
Platform
Operator	METI, NEDO, USEF (Institute for Unmanned Space Experiment Free Flyer)
Mass at launch	980 kg (740 kg?)
Dry Mass	kg
Basic shape	Box + 2 panels
Dimension (m)	10.2 long, 2.5 high
Solar array
Stabilization
DC power
Design lifetime	1 yrs

Decay:

Out of service:	Dec 2011
Cause:

Mission details:

SERVIS (Space Environment Reliability Verification Integrated System) will test the usabilty of COTS elements for the use in space. The mission is financed by Japan′s Ministry of Economy, Trade and Industry (METI), the Organization for New Energy and Industrial Technologies Development (NEDO) and the Institute for Unmanned Space Experiment Free Flyer (USEF).
Utilization of commercial off-the-shelf components in space conditions

Ref.: #7(JR629), #14, #206, #226 - update: 02.12.18