Long March 3#Specifications
{{Short description|Chinese orbital carrier rocket}}
{{distinguish|Long March 3 rocket family}}
{{Infobox rocket
| image = CZ-3 rendering.jpg
| caption = Rendering of Long March 3
|function = Carrier rocket
|manufacturer = CALT
|country-origin= China
|status = Retired
|height = {{convert|43.25|m|ft}}{{cite web|url=http://www.astronautix.com/lvs/cz3.htm|title=CZ-3|author=Mark Wade|publisher=Encyclopedia Astronautica|access-date=2008-04-27|url-status=dead|archive-url=https://web.archive.org/web/20080601101204/http://www.astronautix.com/lvs/cz3.htm|archive-date=2008-06-01}}
|diameter = {{convert|3.35|m|ft}}
|mass = {{convert|204000|kg|lb}}
|stages = 3
|launches = 13
|success = 10
|fail = 2
|partial = 1
|first = 29 January 1984
|last = 25 June 2000
|capacities =
{{Infobox Rocket/Payload
|location=LEO
|kilos = {{convert|5000|kg|lb}}{{cite web|url=http://space.skyrocket.de/doc_lau_det/cz-3.htm|title=CZ-3 (Chang Zheng-3)|author=Gunter Krebs|publisher=Gunter's Space Page|access-date=2008-04-27}}
}}
{{Infobox Rocket/Payload
|location=GTO
|kilos = {{convert|1500|kg|lb}}
}}
|family = Long March
|derivatives= Long March 3A
|stagedata=
{{Infobox rocket/Stage
|type = stage
|stageno = First
|name =
|length = 23.49 m
|diameter = 3.35 m
|empty = {{convert|9378|kg|abbr=on}}
|gross = {{convert|153070|kg|abbr=on}}
|propmass = {{convert|143692|kg|abbr=on}}
|engines = 4 YF-21B
|thrust = {{convert|2961.6|kN|abbr=on}}
|alt-thrust =
|burntime = 121 s
|SI = {{convert|2556.2|m/s|isp|abbr=on}}
}}
{{Infobox rocket/Stage
|type = stage
|stageno = Second
|name =
|length = 9.47 m
|diameter = 3.35 m
|empty = {{convert|3599|kg|abbr=on}}
|gross = {{convert|39440|kg|abbr=on}}
|propmass = {{convert|35841|kg|abbr=on}}
|engines = 1 YF-24D
(1 x YF-22D (Main))
(4 x YF-23F (Vernier))
|thrust = {{convert|741.4|kN|abbr=on}} (Main)
{{convert|47.1|kN|abbr=on}} (Vernier)
|alt-thrust =
|burntime = 130 s
|SI = {{convert|2922.4|m/s|isp|abbr=on}} (Main)
{{convert|2762|m/s|isp|abbr=on}} (Vernier)
}}
{{Infobox rocket/Stage
|type = stage
|stageno = Third
|name =
|length = 10.36 m
|diameter = 2.25 m
|empty = {{convert|1965|kg|abbr=on}}
|gross = {{convert|10700|kg|abbr=on}}
|propmass = {{convert|8731|kg|abbr=on}}
|engines = 1 YF-73
|thrust = {{convert|44.43|kN|abbr=on}}
|alt-thrust =
|burntime = 729 s
|SI = {{convert|4119|m/s|isp|abbr=on}}
|fuel = {{LH2}} / LOX
}}
}}
The Long March 3 ({{zh|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.
List of launches
{{main|List of Long March launches}}
class="wikitable"
! Flight number ! Date (UTC) ! Launch site ! Payload ! Orbit ! Result |
1
|January 29, 1984 |GTO (intended) |{{Partial failure|Partial Failure}} |
2
|April 8, 1984 |LA-3, XSLC |GTO |{{Success}} |
3
|February 1, 1986 |LA-3, XSLC |GTO |{{Success}} |
4
|March 7, 1988 |LA-3, XSLC |GTO |{{Success}} |
5
|December 22, 1988 |LA-3, XSLC |GTO |{{Success}} |
6
|February 4, 1990 |LA-3, XSLC |GTO |{{Success}} |
7
|April 7, 1990 |LA-3, XSLC |GTO |{{Success}} |
8
|December 28, 1991 |LA-3, XSLC |GTO (intended) |{{Failure|Failure}} |
9
|July 21, 1994 |LA-3, XSLC |GTO |{{Success}} |
10
|July 3, 1996 |LA-3, XSLC |GTO |{{Success}} |
11
|August 18, 1996 |LA-3, XSLC |GTO (intended) |{{Failure|Failure}} |
12
|June 10, 1997 |LA-3, XSLC |GTO |{{Success}} |
13
|June 25, 2000 |LA-3, XSLC |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.
Specifications of all LM-3 types
class="wikitable" style="margin: 1em auto 1em auto; text-align:right;"
|+Specifications |style="text-align:left; background:#D9D9D9"|Series |style="text-align:center; background:#edf3fe"|3 |style="text-align:center; background:#edf3fe"|3A |style="text-align:center; background:#edf3fe"|3B |style="text-align:center; background:#edf3fe"|3B/E |style="text-align:center; background:#edf3fe"|3C |style="text-align:center; background:#edf3fe"|3C/E |
style="text-align:left; background:#E6E6E6"|Model |
style="text-align:left; background:#E6E6E6"|Stages
|3 |3 |3 |3 |3 |3 |
style="text-align:left; background:#E6E6E6"|Length (m)
|43.2 |52.5 |54.8 |56.3 |54.8 |56.3 |
style="text-align:left; background:#E6E6E6"|Max. diameter (m)
|3.35 |3.35 |3.35 |3.35 |3.35 |3.35 |
style="text-align:left; background:#E6E6E6"|Liftoff mass (t)
|204 |241 |426 |459 |345 |378 |
style="text-align:left; background:#E6E6E6"|Liftoff thrust (kN)
|2,962 |2,962 |5,923 |5,923 |4,442 |4,442 |
style="text-align:left; background:#E6E6E6"|Payload (LEO, kg)
|5,000 |8,500 |11,500 |11,500 |8,000 |8,000 |
Launch history for all LM-3 types
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 28 May, 2025.
class="wikitable" style="margin: 1em auto 1em auto; text-align:right;"
|+Long March 3 (rocket family) |style="text-align:center; background:#BBB"|Derivatives |style="text-align:center; background:#BBB"|Status |style="text-align:center; background:#BBB"|First flight |style="text-align:center; background:#BBB"|Launches |style="text-align:center; background:#BBB"|Successes |style="text-align:center; background:#BBB"|Failures |style="text-align:center; background:#BBB"|Partial failures |
style="text-align:left;"|Long March 3
|{{site inactive|Retired}} |29 January 1984 |13 |10 |2 |1 |
style="text-align:left;"|Long March 3A
|{{site inactive|Retired}} |8 February 1994 |27 |27 |0 |0 |
style="text-align:left;"|Long March 3B
|{{site inactive|Retired}} |14 February 1996 |12 |10 |1 |1 |
style="text-align:left;"|Long March 3B/E
|{{site active|Active}} |13 May 2007 |97 |95 |1 |1 |
style="text-align:left;"|Long March 3C
|{{site inactive|Retired}} |25 April 2008 |12 |12 |0 |0 |
style="text-align:left;"|Long March 3C/E
|{{site active|Active}} |23 October 2014 |7 |7 |0 |0 |
{{commonscat|Long March 3}}
References
{{reflist}}
{{Portal|Spaceflight|China}}
{{Expendable launch systems}}
{{Chinese space program}}
{{Long March rockets}}