in future.
![](http://zzwave.com/plaboard/uploads/20191204-c900d388-165a-11ea-a2a8-52540010fa16.jpg)
Two configurations. Without booster, LEO 4.5 ton, SSO 3 ton, GTO 0.5 ton. With booster, LEO 8.1 ton, SSO 5 ton, GTO 2.8 ton.
![](http://zzwave.com/plaboard/uploads/20191204-3b35a2d6-165a-11ea-a2a8-52540010fa16-3.jpg)
Design features include automated self diagnosis, simplified launch procedure etc. From order to launch about 12 months, launch preparation about 10 days.
![](http://zzwave.com/plaboard/uploads/20191204-4b7b2148-165a-11ea-a2a8-52540010fa16-3.jpg)
In future, a reusable version will be developed based on CZ-8. Shown here is a core and booster reusable first stage, sharing the same recovery mechanism. The second stage is not resuable.
![](http://zzwave.com/plaboard/uploads/20191204-5829e118-165a-11ea-a2a8-52540010fa16-2.jpg)
Comparing with the European resuable rocket design.
![](http://zzwave.com/plaboard/uploads/20191204-6a9bd43c-165a-11ea-a2a8-52540010fa16-3.jpg)
Concept demonstration of the core and booster stage recovery.
![](http://zzwave.com/plaboard/uploads/20191204-7ab6aa04-165a-11ea-a2a8-52540010fa16.gif)