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SDS 1

NSSDCA/COSPAR ID: 2009-002F

Description

Seven microsatellites were deployed as piggyback payloads to the Ibuki spacecraft. All of these spacecraft will follow a similar roughly 660 km sun-synchronous orbit. Six of the small satellites were developed by universities and private-sector companies; the seventh is a technology demonstrator for JAXA.

SDS 1, the Small Demonstration Satellite 1, is a technology demonstrator mission developed by JAXA. The satellite is approximately 70 x 70 x 60 cm in size and is 100 kg. Solar cells will provide approximately 100 W of power. The spacecraft features a multi-mode integrated transponder. During its mission it will carry out on-orbit verification of a space wire demonstration module, a cutting-edge microprocessor, and a thin-film solar cell.

Facts in Brief

Launch Date: 2009-01-23
Launch Vehicle: H-2A
Launch Site: Tanegashima, Japan

Funding Agency

  • Japan Aerospace Exploration Agency (Japan)

Disciplines

  • Technology Applications
  • Engineering

Additional Information

Questions and comments about this spacecraft can be directed to: Coordinated Request and User Support Office

 
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