Long March 2D

Long March 2D
Rendering of Long March 2D.
FunctionCarrier rocket
ManufacturerSAST
Country of originChina
Cost per launchUS$30 million
Size
Height41.056 m (134.70 ft)
Diameter3.35 m (11.0 ft)
Mass232,250 kg (512,020 lb)
Stages2
Capacity
Payload to LEO
Mass3,500 kg (7,700 lb)
Payload to SSO
Mass1,300 kg (2,900 lb)
Associated rockets
FamilyLong March
Launch history
StatusActive
Launch sitesLA-2/138 and LA-4/SLS-2, JSLC
LA-9, TSLC
LA-3, XSLC
Total launches99
Success(es)98
Partial failure(s)1
First flight9 August 1992
Last flight14 June 2025
First stage
Height27.91 m
Diameter3.35 m
Propellant mass182,000 kg (401,000 lb)
Powered by4 YF-21C
Maximum thrust2,961.6 kN (665,800 lbf)
Specific impulse2,550 m/s (8,400 ft/s)
PropellantN2O4 / UDMH
Second stage
Height10.9 m
Diameter3.35 m
Propellant mass52,700 kg (116,200 lb)
Powered by1 YF-24C
(1 x YF-22C (Main))
(4 x YF-23C (Vernier))
Maximum thrust742.04 kN (166,820 lbf) (Main)
47.1 kN (10,600 lbf) (Vernier)
Specific impulse2,942 m/s (300.0 s) (Main)
2,834 m/s (289.0 s) (Vernier)
PropellantN2O4 / UDMH
Third stage (optional) – YZ-3
Powered by1 × YF-50D
Maximum thrust6.5 kN (1,500 lbf)
Specific impulse315.5 s (3.094 km/s)
PropellantN2O4 / UDMH

The Long March 2D (Chinese: 长征二号丁火箭), also known as the Chang Zheng 2D, CZ-2D, and LM-2D, is a Chinese two-stage orbital carrier rocket mainly used for launching LEO and SSO satellites. It is manufactured by the Shanghai Academy of Spaceflight Technology (SAST).

It is mainly launched from areas LA-2B and LA-4 at the Jiuquan Satellite Launch Center. The Long March 2D made its maiden flight on 9 August 1992. It was initially used to launch FSW-2 and FSW-3 reconnaissance satellites. More recently it has also launched from LA-9 TSLC and LA-3 XSLC.

Unlike all other members of the Long March 2 rocket family, the Long March 2D is a two-stage version of the Long March 4 launch vehicle.