Kibo's Inter-Orbit Communication System (ICS) provides an independent intercommunications network between Kibo and the Tsukuba Space Center (TKSC, JAXA). Commands and voice data are uplinked from the ground through JAXA's Data Relay Test Satellite (DRTS), known as Kodama, to Kibo, and experiment data, image data or voice data are downlinked from Kibo to the ground. The ICS consists of two subsystem components: the ICS-Pressurized Module (ICS-PM) and the ICS-Exposed Facility (ICS-EF). The ICS-PM, which is installed in the PM, will provide command and data handling functions. The ICS-EF is mainly composed of an antenna and pointing mechanism that will be used to communicate with the DRTS.
|Size||2.0×1.0×0.9m||1.1×0.8×2.0m (antenna retracted)
2.2×0.8×2.0m (antenna deployed)
|Data rate /
|Downlink||50Mbps / About 26GHz|
|Uplink||3Mbps / About 23GHz|
|DRTS communication window*||Total of 7.8 hours per day (DRTS currently consists of only one satellite)
Max. 40min. per orbit
The following are details of the ICS subsystems, ICS-PM and ICS-EF components.
The ICS Pressurized Module (ICS-PM) is installed in the ICS rack that was delivered to the International Space Station (ISS) on the STS-123 Mission (1J/A). The ICS-PM multiplexes the Kibo's systems and experiment data for downlink to the ground, and demultiplexes the data uplinked from the ground. Also, the ICS-PM modulates the data before sending, and demodulates the data after receipt. The ICS-PM has an automatic operation scheduling function where commands are uplinked from the ground in advance while the DRTS is in a communication window. The ICS-PM also has a data recording function for later downloading to the ground, whenever real-time communication is not available.
The ICS Exposed Facility (ICS-EF) comprises several components, including an anntenna, pointing mechanism, frequency converters, high-power amplifier, and various sensors including the Earth sensor, Sun sensor, and inertial reference unit. The ICS antenna can automatically track the DRTS.
The ICS-PM was installed in the ICS Rack and delivered to the ISS on the STS-123 Mission. The ICS Rack was installed in the PM during the STS-124 Mission (1J).
The ICS-EF was launched on the STS-127 Mission (2J/A).
|Copyright 2007 Japan Aerospace Exploration Agency||Site Policy|