Servis 1

Space Environment Reliability Verification Integrated System

---

General

Designation	28060 / 03050A
Launch date	30 Oct 2003
Country of origin	Japan
Mission	Technology
Perigee/Apogee	1000 km, sun-synchronous
Inclination	99.5°
Period	105 min
Launch vehicle	Rokot #10

Owned by the institute for Unmanned Space Experiment Free Flyer (Japan).

Will evaluate COTS components in space environment and a lithium-ion battery.

---

External resources

http://www.usef.or.jp/english/f3_project/servis/f3_servis.html

sat-index articles

Technical data

---

---

Specifications

Prime contractor	Melco
Platform
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 years

---