![]() The first stage of the SS-520 is based on the S-520 rocket, with a smaller second stage mounted atop it to increase the maximum altitude the rocket can reach on suborbital missions. SS-520-4 will make the third flight of the SS-520, which first flew on 5 February 1998 from Uchinoura and made a second launch in December 2000 from Svalbard, Norway, carrying out geomagnetic research missions. The SS-520 is a two-stage solid-fuelled sounding rocket, designed to carry research payloads on suborbital missions to altitudes of around 800 to 1,000 kilometers (620 miles, 540 nautical miles).įor the mission, which has the flight designation SS-520-4, the vehicle has been modified with the addition of a small third stage to inject its payload into a low Earth orbit. The TRICOM-1 satellite is a CubeSat, carrying a communications experiment and cameras for Earth imaging. Japanese Launch:Ī one-off demonstration mission, the launch aimed to prove the concept of using a minimally-modified sounding rocket to place small satellites into orbit.īoth IHI Aerospace and Canon have investigated partnerships with the Japan Aerospace Exploration Agency (JAXA) on the development of rockets to launch small satellites, and the launch will gather data which could aid these programs. However, the launch has been declared as a failure. The mission lifted off from the Uchinoura Space Centre at 08:33 local time (23:33 UTC on Saturday), aiming to mark a new record for small rocket launch capability. Japan conducted an experimental launch, using a modified SS-520 sounding rocket to place a CubeSat, TRICOM-1, into low Earth orbit.
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