YZ-1A R/B

China

Int. spacecraft nº:

Chinese spacecraft nº: 296

Also called: ZGZ Shiyan Zhuangzhi

Launch data:

Designation	41624 / 16042A
Launch date - time	25 June 2016 - 12:00 UT
Launch site	Wenchang, LC201
Launch vehicle	CZ-7/YZ1
Mission	Technology
Earth orbit:
Perigee / Apogee	287 x 381 km
Eccentricity
Inclination	40.8 °
Period	min

First launch Rocket
Launched together with: DFFC - Aoxiang Zhixing - Tiange Feixingqi 1 & 2 - Aolong 1

Spacecraft data:

Prime manufacturer
Platform	Experiment mounted on YZ-1A upper stage
Operator
Mass at launch	kg
Dry Mass	kg
Basic shape
Dimension (m)
Equipment
Solar array	Solar cells
Stabilization
Propulsion
DC power

End of live:

Re-entered date:	27 June 2016
Lifetime:

Description:

The ZGZ Shiyan Zhuangzhi (Zai Guijia Zhu Shiyan Zhuangzhi) or In-Orbit Refeulling Experimental Device is a fluid-transfer experiment.
The experiment is mounted on the YZ-1A upper stage and remains attached. After the experiments, it is to deorbited with the upper stage.

Mission details:

Deployement see: DFFC
Attached to the YZ-1A as a non-separable payload is the 'zai guijia zhu shiyan zhuangzhi', the In-Orbit Refeulling Experimental Device.

Ref.: #7(JR727), #14, #228 - update: 04.03.17