High End China Satellite Support Services Equipment Manufacturing

Remote Sensing Satellite

R&D Level

In terms of satellite R&D, in accordance with the judgment of satellite technology development trend and commercial development mode, the core technical team has broken through the traditional design concept and adopted the technical route of "satellite platform and load integration". After four times of progress in ten years, the weight of the satellite has been reduced to 20kg from 400kg of the initial generation.

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Optical Processing Area

Production Conditions

The total area of the optical processing area is 10000m2. This area is capable of undertaking the mass production of high-precision optical components, and has the ability to process optical components made of glass ceramics and silicon carbide, etc. from coarse to fine, as well as corresponding detection.

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Dec, 25

Application of the 3U Standard Platform in the KAUSAT-5 CubeSat

This research completed the design and development of KAUSAT-5 by applying the standard platform. KAUSAT-5 is a 3U (100×100×340mm³) CubeSat capable of performing multiple scientific missions and technology verification tasks.

Dec, 25

Subsystem Design of the 3U Standard Platform—MDHS (Mission Data Handling Subsystem) and CS (Communication Subsystem)

The MDHU (Mission Data Handling Unit) in the MDHS (Mission Data Handling Subsystem) is primarily responsible for processing and storing mission data, and transmitting the data to the ground via the S-band.

Dec, 25

Subsystem Design of the 3U Standard Platform—EPS (Electrical Power Subsystem)

The EPS (Electrical Power Subsystem) of the standard platform is required to provide sufficient power for the satellite's payload and platform during the satellite mission, ensuring the smooth execution of the mission.

Dec, 25

Subsystem Design of the 3U Standard Platform—ADCS (Attitude Determination and Control Subsystem)

The ADCS (Attitude Determination and Control Subsystem) of the standard platform is equipped with MTQ (Magnetorquer), MEMS (Micro-Electro-Mechanical Systems) IMU (Inertial Measurement Unit), and MEMS magnetic sensors for the sensing and actuation of satellite attitude.

Dec, 25

Subsystem Design of the 3U Standard Platform—SMS (Structure and Mechanism Subsystem)

The core function of the SMS (Structure and Mechanism Subsystem) is to support the satellite's platform and payload, and protect the satellite from external environmental impacts throughout the entire process from launch to entering space.

Dec, 25

Configuration and Parameter Selection of the 3U CubeSat Standard Platform

The number of 3U CubeSats corresponds to the space (volume) occupied by the platform within the 3U CubeSat system.

Dec, 25

Structure of the 3U CubeSat Standard Platform

The standard platform is based on an optimized lightweight and modular design to reduce the overall development cost and cycle of the satellite.

Dec, 25

Core Concepts of the 3U CubeSat Standard Platform

The core goal of the standard platform is to meet diverse mission requirements with minimal modifications, where the modularity and reconfigurability of each component are crucial.