Japan Aerospace Exploration Agency (JAXA)
The Venus Climate Orbiter "AKATSUKI," which was launched on May 21, 2010 (Japan Standard Time,) turned on the orbital maneuvering engine (OME) to jet 500 Newton (N)*1 of thruster on June 28 (JST) at a distance of 14.6 million km from the earth or 1.06 astronomical units (AU)*2 from the sun. As a result, we have successfully performed on-orbit verification of the ceramic thruster, made of silicon nitride (Si3N4) for the first time in the world. The thruster was newly developed in Japan.
Image: Onboard position of the 500 N class ceramic thruster, whose on-orbit verification was successfully performed.
This thruster is a liquid rocket engine using hydrazine and nitrogen peroxide, and it is mainly used for retrofiring when the orbiter is injected into the Venus orbit. The thrust emitted this time is not only for adjusting the access to Venus, but is also an imperative operation to evaluate the thrust characteristics of the engine for Venus orbit insertion. As a result of our detailed orbit tracking by the JAXA Uchinoura Space Center, JAXA Usuda Deep Space Center, and NASA Deep Space Network (DSN) stations, we have confirmed that about 12 meters per second of velocity correction was performed by 13-second firing of the OME, and that met the range of the scheduled orbit control. The next orbit control (fine adjustment) is scheduled in early November, and AKATSUKI will go to the nearest point of Venus and be injected into the Venus orbit on December 7 (JST.)
Currently, the explorer and its onboard devices are working properly, and the Ultra-Stable Oscillator (USO) was also found to be functioning well to achieve the frequency stability as expected in addition to the Ultraviolet Imager (UVI,) 1µm Camera (IR1) and Longwave IR Camera (LIR,) whose initial functional verifications were already completed on the launch day evening.