Satellite | ZDPS 1A |
---|---|
Form factor | Nanosatellite |
Units or mass | 3.5 kg |
Entity name | Zhejiang University |
Institution | University |
Entity type | Academic / Education |
Country | China |
Oneliner |
Demonstrate platform technologies with focus on camera, COTS components and ADCS. |
Description |
Platform verification. The functionality, performance and space environmental adaption of the satellites and their subsystems were to be validated in space via on-orbit testing and operation. Experimentation of miniaturized parts. Micro panoramic camera. Momentum wheel is employed to offer gyro stiffness stability in the pitch |
Sources | [1] |
Photo sources | [1] [2] |
Space photos |
Related Spacecraft
Spacecraft | Status | Rocket | Launch | Orbit |
---|---|---|---|---|
ZDPS 1A 01 (Zheda Pixing, Pixing 1) | Was operational until XXXX-XX-XX, more than 2 years? | Long March 2D | 2010-09-22 | 650 km, 98.2 deg, SSO |
ZDPS 1A 02 (Zheda Pixing, Pixing 1) | Was operational until XXXX-XX-XX, more than 2 years? | Long March 2D | 2010-09-22 | 650 km, 98.2 deg, SSO |
Last modified: 2023-06-08