Kaituozhe-1
Kaituozhe familyChina Aerospace Science and Industry CorporationRetired
A small solid fueled launch vehicle based on the road mobile DF-21 IRBM with an additional upper stage.
Specifications
- Height
- 18 m
- Diameter
- 2 m
- Launch mass
- 20 t
- Stages
- 4
- LEO capacity
- 100 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
0%success rate0 of 3
3failuresincluding partial failures
0success streakcurrent
First flight September 15, 2002 · latest June 9, 2005
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Kaituozhe-1 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2002 | 0 | 1 | 1 |
| 2003 | 0 | 1 | 1 |
| 2004 | 0 | 0 | 0 |
| 2005 | 0 | 1 | 1 |