Long March 3

	Long March 3
Function	Carrier rocket
Manufacturer	CALT
Country of origin	China
Size
Height	43.25 metres (141.9 ft)
Diameter	3.35 metres (11.0 ft)
Mass	204,000 kilograms (450,000 lb)
Stages	3
Capacity
Payload to LEO
Mass	5,000 kilograms (11,000 lb)
Payload to GTO
Mass	1,500 kilograms (3,300 lb)
Associated rockets
Family	Long March
Derivative work	Long March 3A
Launch history
Status	Retired
Launch sites	LA-3, XSLC
Total launches	13
Success(es)	10
Failure(s)	2
Partial failure(s)	1
First flight	29 January 1984
Last flight	25 June 2000
First stage
Height	23.49 m
Diameter	3.35 m
Empty mass	9,378 kg (20,675 lb)
Gross mass	153,070 kg (337,460 lb)
Propellant mass	143,692 kg (316,787 lb)
Powered by	4 YF-21B
Maximum thrust	2,961.6 kN (665,800 lbf)
Specific impulse	2,556.2 m/s (260.66 s)
Burn time	121 s
Propellant	N2O4 / UDMH
Second stage
Height	9.47 m
Diameter	3.35 m
Empty mass	3,599 kg (7,934 lb)
Gross mass	39,440 kg (86,950 lb)
Propellant mass	35,841 kg (79,016 lb)
Powered by	1 YF-24D; (1 x YF-22D (Main)); (4 x YF-23F (Vernier))
Maximum thrust	741.4 kN (166,700 lbf) (Main); 47.1 kN (10,600 lbf) (Vernier)
Specific impulse	2,922.4 m/s (298.00 s) (Main); 2,762 m/s (281.6 s) (Vernier)
Burn time	130 s
Propellant	N2O4 / UDMH
Third stage
Height	10.36 m
Diameter	2.25 m
Empty mass	1,965 kg (4,332 lb)
Gross mass	10,700 kg (23,600 lb)
Propellant mass	8,731 kg (19,249 lb)
Powered by	1 YF-73
Maximum thrust	44.43 kN (9,990 lbf)
Specific impulse	4,119 m/s (420.0 s)
Burn time	729 s
Propellant	LH2 / LOX
	[edit on Wikidata]

The Long March 3 (Chinese: 长征三号火箭), also known as the Changzheng 3, CZ-3 and LM-3, was a Chinese orbital carrier rocket design. They were all launched from Launch Area 3 at the Xichang Satellite Launch Center. It was a 3-stage rocket, and was mostly used to place DFH-2-class communications satellites into geosynchronous transfer orbits. It was complemented and later replaced by the more powerful Long March 3A, which has an improved third stage.

List of launches

Flight number	Date (UTC)	Launch site	Payload	Orbit	Result
1	January 29, 1984 12:25	LA-3, XSLC	STTW 1	GTO (intended)	Partial Failure
2	April 8, 1984 11:20	LA-3, XSLC	STTW 2	GTO	Success
3	February 1, 1986 12:37	LA-3, XSLC	DFH-2-1	GTO	Success
4	March 7, 1988 12:41	LA-3, XSLC	DFH-2A-1 (ChinaSat 1)	GTO	Success
5	December 22, 1988 12:40	LA-3, XSLC	DFH-2A-2 (ChinaSat 2)	GTO	Success
6	February 4, 1990 12:28	LA-3, XSLC	DFH-2A-3 (ChinaSat 3)	GTO	Success
7	April 7, 1990 13:30	LA-3, XSLC	AsiaSat 1	GTO	Success
8	December 28, 1991 12:00	LA-3, XSLC	DFH-2A-4 (ChinaSat 4)	GTO (intended)	Failure
9	July 21, 1994 10:55	LA-3, XSLC	APStar 1	GTO	Success
10	July 3, 1996 10:47	LA-3, XSLC	APStar 1A	GTO	Success
11	August 18, 1996 10:27	LA-3, XSLC	ChinaSat 7	GTO (intended)	Failure
12	June 10, 1997 12:01	LA-3, XSLC	Fengyun 2A	GTO	Success
13	June 25, 2000 11:50	LA-3, XSLC	Fengyun 2B	GTO	Success

Launch failures

Dong Fang Hong 2 launch failure

On January 29, 1984, a LM-3 rocket failed during launch. The third stage failed 4 s after restart for GTO insertion of the satellite, due to incorrect mixture ratio in the engine gas generator, which caused high temperatures and burned out the turbine casing. However, many planned tests on the experimental communications spacecraft were still carried out in the resulting elliptical orbit.

ChinaSat 4 launch failure

On December 28, 1991, a LM-3 rocket failed during launch. The third-stage engine suffered a loss of turbine speed and combustion pressure 58 s after re-igniting for the second burn for GTO insertion and shut down completely 135 s after re-ignition. Loss of pressure in the high-pressure helium supply used for engine control had reduced the propellant flow.

ChinaSat 7 launch failure

On August 18, 1996 a LM-3 rocket failed during launch. The third-stage engine shut down roughly 40 s earlier than planned because of a fire in the LH2 injector of the gas generator. Insufficient purging had permitted oxygen to freeze in the gas generator during flight.

References

^ ^a ^b ^c Mark Wade. "CZ-3". Encyclopedia Astronautica. Archived from the original on 2008-06-01. Retrieved 2008-04-27.
^ ^a ^b Gunter Krebs. "CZ-3 (Chang Zheng-3)". Gunter's Space Page. Retrieved 2008-04-27.

[EA-1] Mark Wade. "CZ-3". Encyclopedia Astronautica. Archived from the original on 2008-06-01. Retrieved 2008-04-27.

[GSP-2] Gunter Krebs. "CZ-3 (Chang Zheng-3)". Gunter's Space Page. Retrieved 2008-04-27.

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v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H 12 LVM3 Minotaur I IV V C Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Deca Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 Miura 5 MLV Neutron New Glenn New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 RS1^† Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^†
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

v t e Long March (rocket family)
Rockets	Feng Bao 1 Long March 1 1D Long March 2 2A 2C 2D 2E 2F Long March 3 3A 3B 3B/E 3C Long March 4 4A 4B 4C Long March 5 5B Long March 6 6A 6C Long March 7 7A Long March 8 8A Long March 9 Long March 10 Long March 11 11H Long March 12
Launch sites	Jiuquan Taiyuan Wenchang Commercial Xichang
Manufacturers	China Academy of Launch Vehicle Technology Shanghai Academy of Spaceflight Technology
Designers	Wang Xiji
List of Long March launches