Long March 2E
Long March family · China Aerospace Science and Technology Corporation · Retired
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
- Launch cost
- —
- LEO capacity
- 9,200 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
7
Launches with a definitive outcome
Success rate
71.4%
5 of 7
Current success streak
2
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
- Long March 2E | Echostar I — Success
- Long March 2E | Asiasat 2 — Success
- Long March 2E | Apstar 2 — Failure
- Long March 2E | Optus B3 — Success
- Long March 2E | Optus B2 — Failure