Xiaoxiang 1 [CGTRI]
Xiaoxiang 1 (XX 1) is a developed at the Changsha Gaoxinqu Tianyi Research Institute, Hunan.
The 8 kg satellite is built to the 6U CubeSat form factor. The payload consists of a stabilization system to provide precise, stabilzed camera pointing.
Xiaoxiang 1 was launched as a piggy-back payload on the second flight of the CZ-11 rocket.
|Type / Application:||Technology|
|Operator:||Changsha Gaoxinqu Tianyi Research Institute, Hunan|
|Contractors:||Changsha Gaoxinqu Tianyi Research Institute, Hunan|
|Equipment:||Stabilized camera system|
|Power:||2 deployable fixed solar arrays, batteries|
|Orbit:||500 km SSO|
|Xiaoxiang 1||2016-066B||09.11.2016||Jq SLS-E2||CZ-11||with XPNAV 1, Lishui 1-01, Pina-2 01, Pina-2 02, CAS 2T & KS 1Q|