Rubin 3

Also called Rubin-3-DSI

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General

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

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External resources

sat-index articles

http://www.ohb-system.de/Satellites/Missions/rubin3.html

Technical data

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Specifications

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

It communicates by email via the Orbcomm network.

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