NanoACE |
USA |
Int. spacecraft nº: |
US spacecraft nº: |
Launch data:
|
| ||||||||||||||||||||
| Prime manufacturer | Tyvak Nano-Satellite Systems, Inc. |
| Platform | 3U cubesat |
| Operator | Tyvak Nano-Satellite Systems, Inc. |
| Mass at launch | 5,2 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension | 30 x 10 x 10 cm |
| Equipment | 2 IR cameras, 2 visible cameras |
| Solar array | Solar cells |
| Stabilization | |
| Propulsion | 8 cold gas thrusters |
| DC power | |
| Design lifetime | 1 y |
| Ref.: #7(JR740, #14) - update: 16.01.18 | Home |