 |
The LM-2D launch vehicle is developed and manufactured by Shanghai Academy of Spaceflight Technology(SAST), a subsidiary of CASC. It is a two-stage liquid carrier rocket, using N2O4 and UDMH as the propellant on its first and second stages. The payload capability of LM-2D for 700km SSO is 1.2 tons. The LM-2D launch vehicle has conducted 31 successful launch missions so far.
LM-2D FLIGHT SEQUENCE
No. |
Time (s) |
Flight Events |
1 |
0.000 |
Lift-off |
2 |
156.659 |
1st/2nd Stage Separation |
3 |
195.659 |
Fairing jettison |
4 |
322.590 |
2nd stage main engine shutdown |
5 |
747.700 |
2nd stage vernier engine shutdown |
6 |
779.700 |
SC/LV Separation |
|