Long March 2E
Long March familyChina Aerospace Science and Technology CorporationRetired
The Long March 2E is a斯expendable launch vehicle made and operated by China. It is a two stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethylhydrazine, augmented by 4 liquid fuel boosters using the same fuel.
Specifications
- Thrust
- 5,923 kN
- Height
- 49.686 m
- Diameter
- 7.85 m
- Launch mass
- 462 t
- Stages
- 3
- LEO capacity
- 9,200 kg
- GTO capacity
- 3,500 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
7flightswith a definitive outcome
71.4%success rate5 of 7
2failuresincluding partial failures
2success streakcurrent
First flight July 16, 1990 · latest December 28, 1995
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Long March 2E flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1990 | 1 | 0 | 1 |
| 1991 | 0 | 0 | 0 |
| 1992 | 1 | 1 | 2 |
| 1993 | 0 | 0 | 0 |
| 1994 | 1 | 0 | 1 |
| 1995 | 2 | 1 | 3 |