Kaituozhe-1
Kaituozhe family · China Aerospace Science and Industry Corporation · Retired
A small solid fueled launch vehicle based on the road mobile DF-21 IRBM with an additional upper stage.
Specifications
- Thrust
- —
- Height
- 18 m
- Diameter
- 2 m
- Launch mass
- 20 t
- Stages
- 4
- Launch cost
- —
- LEO capacity
- 100 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
3
Launches with a definitive outcome
Success rate
0%
0 of 3
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Kaituozhe-1 | KT-1 satellite? — Failure
- Kaituozhe-1 | Hangtian Tsinghua 1-02 — Failure
- Kaituozhe-1 | Hangtian Tsinghua 1-01 — Failure