Techsat 1

Also called Gurwin 1

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General

Launch date	28 Mar 1995
Country of origin	Israel
Mission	Telecommunications
Launch vehicle	Start #2

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End of life

Cause	Launcher failure
Decay	28 Mar 1995

The satellite carried a CCD camera, a radiation detector, an ozone monitor as well as satellite technology tests. It carried a multi-user store-and-forward Amateur Radio digital communications transponder. Gurwin could primarily operate at 9600 bits per second FSK although it was also capable of 1200 bps BPSK.

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External resources

http://www.technion.ac.il/pub/projects/techsat/

Technical data

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Specifications

Prime contractor	Technion-Israel Institute of Technology in Haifa
Platform
Mass at launch	50 kg
Mass in orbit
Length	0.45 m
Width	0.5 m
Height	0.5 m
Stabilization
DC power
Design lifetime

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Frequency chart

145 MHz uplink	1269 MHz uplink	435 MHz downlink
145.850	1269.700	435.225
145.890	1269.800	435.325
145.910	1269.900
145.930	1269.950

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