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Overview

IKAROS is a small-scale demonstration satellite that uses solar power generated via thin film solar cells attached to its sail, called a solar sail because it captures the sun's energy to propel itself. This experiment verified that the satellite could be accelerated with solar power while it was also possible to control the trajectory of the satellite with LCD devices and verify navigational technology that made use of the solar sail. IKAROS was launched on May 21, 2010, on an H-IIA rocket and successfully demonstrated solar sail propulsion, power generation via thin film solar cells, and trajectory control capabilities.

Key facts

Payload
Reach
Speed
Weight
310 kg
IP rating
Battery
Power
Autonomy
fully autonomous
Launch year
2010
Price
Status
active

Detailed specifications

Other2
Deployment Count
1
Deployment Notes
Deployed in two stages: first quasi-statically by onboard mechanism, then dynamically using centrifugal force from spinning at up to 20 rpm[1][2].

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