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+---------------------------------------------------------------------------+ | Payload | +---------------------------------------------------------------------------+ | Science Instrument | Task | +---------------------------------------------------------------------------+ | Low Energy Concentrator | X-ray spectrometry/imaging in the | | Spectrometer (LECS) | 0.1-10 keV energy range | +---------------------------------------------------------------------------+ | Medium Energy Concentrator | X-ray spectrometry/imaging in the | | Spectrometer (MECS) | 1-10 keV energy range | +---------------------------------------------------------------------------+ | High Pressure Gas Scintillation | X-ray spectrometry in the 3-120 keV | | Proportional Counter (HP-GSPC) | energy range | +---------------------------------------------------------------------------+ | Phoswich Detector System (PDS) | X-ray spectrometry in the 15-300 | | | keV energy range and Gamma-ray | | | burst monitoring in the 60-600 keV | | | energy range | +---------------------------------------------------------------------------+ | Wide Field Cameras (WFCs) | X-ray spectrometry/imaging in the | | | 2-30 keV energy range | +---------------------------------------------------------------------------+ +---------------------------------------------------------------------------+ | Spacecraft | +---------------------------------------------------------------------------+ | Subsystem | Task | +---------------------------------------------------------------------------+ | Structure (STS) | Holding all spacecraft subsystems | | | and science instruments | +---------------------------------------------------------------------------+ | Thermal Control (TCS) | Ensuring temperature ranges and | | | gradients during all mission phases | +---------------------------------------------------------------------------+ | Harness (HRNS) | Electrical interconnection | +---------------------------------------------------------------------------+ | On Board Data Handling (OBDH) | On board data storage and | | | communication management | +---------------------------------------------------------------------------+ | Telemetry Tracking & Commands (TT&C)| Commanding and telemetry data | | | transmission through RF link | +---------------------------------------------------------------------------+ | Attitude and Orbit Control (AOCS) | Satellite attitude determination | | | and pointing to the selected sources| +---------------------------------------------------------------------------+ | Reaction Control (RCS) | Thrusting capability for orbit | | | recovery | +---------------------------------------------------------------------------+ | Electrical Power (EPS) | Energy storage, voltage regulation, | | | power switching and distribution | +---------------------------------------------------------------------------+ | Solar Array (SAS) | Power supply during sunlight phase | +---------------------------------------------------------------------------+ | Electrical Ground Support | H/W and S/W to support integration | | Equipment (EGSE) | and testing of the satellite | +---------------------------------------------------------------------------+