Spacecraft
The Arase spacecraft is the second satellite based on SPRINT bus, after Hisaki (satellite), Hisaki (SPRINT-A). Arase weighs about 350 kg, measures about 1.5 m × 1.5 m × 2.7 m at launch. Once in orbit, it will extend four solar panels, two 5 m masts, and four 15 m wire antennas. The spacecraft is spin-stabilized at 7.5 rpm (8 seconds). Planned mission duration was for one year of scientific observation, but the mission remains active over 5 years later.Launch
Arase's launch on the enhanced Epsilon (rocket), Epsilon's maiden flight was originally scheduled for 2015, but was postponed to the 2016 financial year due to satellite development delays.Instruments
Arase carries following instruments: * XEP-e (Extremely high-energy electron sensor) * HEP-e (High-energy particle sensor – electron) * MEP-e (Medium-energy particle sensor – electron) * LEP-e (Low-energy particle sensor – electron) * MEP-i (Medium-energy particle – ion) * LEP-i (Low-energy particle – ion) * MGF (Magnetic Field Experiment) * PWE (Plasma Wave Experiment) * S-WPIA (Software Wave-Particle Interaction Analyzer) MGF is located at the end of 5 m extended mast. PWE consists of a search coil (PWE-MSC) located at the end of another 5 m extended mast, four 15 m wire antennae (PWE-WPT), and associated electronics unit (PWE-E). S-WPIA will analyse the data obtained by other instruments.See also
* Akebono (satellite), AkebonoReferences
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