Search
 

 

LM- 3B Launch Vehicle

* History

To meet the demand of worldwide communications satellite market, the development of LM-3B launch vehicle was started in 1986, based on the flight proven technology of Long March launch vehicles. In April of 1992, Intelsat executed a launch services contract with CGWIC to use an LM-3B to launch Intelsat 708 communications satellite. It indicated that the LM-3B development entered a new development stage and the LM-3B configuration had been acceptable by world launch services industry.

Unfortunately, the maiden flight of LM-3B launch failed because the inertial reference altered. After investigation and corrections to the failure of the maiden flight, the LM-3B launch vehicle achieved five consecutive successes. The LM-3B launch vehicle has been proven to be a mature powerful launch vehicle in the Long March family.

* Technical Data

LM-3B launch vehicle is the most powerful launch vehicle in Long March fleet based on the LM-3A as the core stage with four liquid boosters strapped on the first stage. The development of LM-3B has been made upon the extensive heritage of the mature and flight proven technology of Long March family of launch vehicles. It is specially dedicated for launching heavyweight communications satellite for GTO missions. The GTO launch capability of LM-3B is 5,100kg.

 

 

Booster

1stStage

2ndStage

3rdStage

Stage Diameter (m)

2.25

3.35

3.35

3.00

Stage Length (m)

15.326

23.272

9.943

12.375

Mass of Propellants (t)

37.746¡Á4

171.775

49.605

18.193

Propellant

N2O4/UDMH

LOX/LH2

Engine

DaFY5-1

DaFY6-2

DaFY20-1 (Main)
DaFY20-1(Vernier)

YF-75

Engine Thrust (KN)

740.4¡Á4

2961.6

742 (Main)
11.8¡Á4 (Vernier)

78.5¡Á2

Engine Specific Impulse
(N¡¤Sec/kg)

2556.2

2556.2

2922.57(Main)
2910.5(Vernier)

4312

Booster

4

Lift-off Mass (t)

426

Overall Length (m)

54.838

Fairing Diameter (m)

4.00/4.20

Fairing Length (m)

9.56

GTO Launch Capacity (kg)

5100

 

Launch Record

(As of April 30, 2005)

No.

Launch Vehicle

Launch Date

Payload

Mission

LaunchCenter

Result

1

LM-3B F01

15 Feb. 96

INTELSAT-7A

GTO

XSLC*

Failure

2

LM-3B F02

20 Aug. 97

MABUHAYSAT

GTO

XSLC

Success

3

LM-3B F03

17 Oct. 97

APSTAR-II R

GTO

XSLC

Success

4

LM-3B F04

30 May 98

ChinaStar-1

GTO

XSLC

Success

5

LM-3B F05

18 July 98

SinoSat-1

GTO

XSLC

Success

6

LM-3B F06

12 April 05

APSTAR-VI

GTO

XSLC

Success

Note:
* Xichang Satellite Launch Center.

 

LM- 2C/CTS Launch Vehicle LM- 2D Launch Vehicle LM- 2E Launch Vehicle
LM- 3A Launch Vehicle LM- 3B Launch Vehicle LM- 4 Launch Vehicle