picture of the encyclopedia
previous next
Version 0.81 comes with a new web design! Please allow popups for navigation.

Rubin 3

Also called Rubin-3-DSI


Designation 27561 / 02054C
Launch date 28 Nov 2002
Country of origin Germany
Mission Technology
Perigee/Apogee 681/742 km
Inclination 98.2°
Launch vehicle Cosmos C

It remained attached to the rocket's payload adapter.

Was developed by OHB-System in co-operation with the University of Applied Sciences, Bremen and the Russian company KB POLYOT, Omsk. Recorded launch vehicle flight data.

External resources

sat-index articles


Technical data


Prime contractor OHB
Mass at launch 45 kg
Mass in orbit  
Solar array  
Stabilization none
DC power 45 W solar cells
Design lifetime  

It communicates by email via the Orbcomm network.

© TBS Internet, all rights reserved. All reproduction, copy or mirroring prohibited. Legal notice
francais anglais contact