Long March 3
Rendering of Long March 3 | |
| Function | Medium-lift launch vehicle |
|---|---|
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | China Academy of Launch Vehicle Technology |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | China |
| Size | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 43.25 metres (141.9 ft)[1] |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 3.35 metres (11.0 ft)[1] |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 204,000 kilograms (450,000 lb)[1] |
| Stages | 3 |
| Capacity | |
| Payload to LEO | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 5,000 kilograms (11,000 lb)[2] |
| Payload to GTO | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 1,500 kilograms (3,300 lb)[2] |
| Associated rockets | |
| Family | Long March |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | Long March 3A |
| Launch history | |
| Status | Retired |
| Launch sites | LA-3, XSLC |
| Total launches | 13 |
| Success(es) | 10 |
| Failure | 2 |
| Partial failure | 1 |
| First flight | 29 January 1984 |
| Last flight | 25 June 2000 |
| First stage | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 23.49 m |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 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) |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 4 YF-21B |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 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 | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 9.47 m |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 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) |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 1 YF-24D (1 x YF-22D (Main)) (4 x YF-23F (Vernier)) |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 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 | |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 10.36 m |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 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) |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 1 YF-73 |
| Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value). | 44.43 kN (9,990 lbf) |
| Specific impulse | 4,119 m/s (420.0 s) |
| Burn time | 729 s |
| Propellant | LH2 / LOX |
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 three-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.
Launch statistics
[edit | edit source]Original LM 3 only.
- Failure
- Partial failure
- Success
- Planned
List of launches
[edit | edit source]| Flight number | Date (UTC) | Launch site | Payload | Orbit | Result |
|---|---|---|---|---|---|
| 1 | 29 January 1984 12:25 |
LA-3, XSLC | STTW 1 | GTO (intended) | Partial Failure |
| 2 | 8 April 1984 11:20 |
LA-3, XSLC | STTW 2 | GTO | Success |
| 3 | 1 February 1986 12:37 |
LA-3, XSLC | DFH-2-1 | GTO | Success |
| 4 | 7 March 1988 12:41 |
LA-3, XSLC | DFH-2A-1 (ChinaSat 1) | GTO | Success |
| 5 | 22 December 1988 12:40 |
LA-3, XSLC | DFH-2A-2 (ChinaSat 2) | GTO | Success |
| 6 | 4 February 1990 12:28 |
LA-3, XSLC | DFH-2A-3 (ChinaSat 3) | GTO | Success |
| 7 | 7 April 1990 13:30 |
LA-3, XSLC | AsiaSat 1 | GTO | Success |
| 8 | 28 December 1991 12:00 |
LA-3, XSLC | DFH-2A-4 (ChinaSat 4) | GTO (intended) | Failure |
| 9 | 21 July 1994 10:55 |
LA-3, XSLC | APStar 1 | GTO | Success |
| 10 | 3 July 1996 10:47 |
LA-3, XSLC | APStar 1A | GTO | Success |
| 11 | 18 August 1996 10:27 |
LA-3, XSLC | ChinaSat 7 | GTO (intended) | Failure |
| 12 | 10 June 1997 12:01 |
LA-3, XSLC | Fengyun 2A | GTO | Success |
| 13 | 25 June 2000 11:50 |
LA-3, XSLC | Fengyun 2B | GTO | Success |
Launch failures
[edit | edit source]Dong Fang Hong 2 launch failure
[edit | edit source]On 29 January 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
[edit | edit source]On 28 December 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
[edit | edit source]On 18 August 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.
Including other LM-3 variants
[edit | edit source]Specifications of all LM-3 types
[edit | edit source]Launch history for all LM-3 types
[edit | edit source]The following launch statistics are gathered from the individual Wikipedia pages of each CZ-3x variants as those pages are updated more frequently by various editors; the numbers are current as of 15 December 2025.
| Derivatives | Status | First flight | Launches | Successes | Failures | Partial failures |
| Long March 3 | Retired | 29 January 1984 | 13 | 10 | 2 | 1 |
| Long March 3A | Retired | 8 February 1994 | 27 | 27 | 0 | 0 |
| Long March 3B | Retired | 14 February 1996 | 12 | 10 | 1 | 1 |
| Long March 3B/E | Active | 13 May 2007 | 101 | 99 | 1 | 1 |
| Long March 3C | Retired | 25 April 2008 | 12 | 12 | 0 | 0 |
| Long March 3C/E | Active | 23 October 2014 | 8 | 8 | 0 | 0 |
References
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