.jpg "ZDPS 1A")
| 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 | 
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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
