Main body of the spacecraft is a box shape of 1.6 m x 1.25 m x 1.6 m with the orbital maneuvering engine (OME) of 450 mm in length. ... 2 shows a block diagram of the entire system. ... (AOCS) consists of reaction wheels (RW), an inertial reference unit with gyros (IRU), star trackers (STT), sun sensors (TSAS and CSAS), accelerometers (ACM), ... I Advances in Space Research 34 (2004) 1668-1672 1669.
|Title||:||Planetary ionospheres and atmospheres including CIRA|