Long March 2F

Chinese rocket From Wikipedia, the free encyclopedia

The Long March 2F (Chinese: 长征二号F火箭 Changzheng 2F), also known as the CZ-2F, LM-2F and Shenjian (神箭, "Divine Arrow"),[1] is a Chinese orbital carrier rocket, part of the Long March 2 rocket family. Designed to launch crewed Shenzhou spacecraft, the Long March 2F is a human-rated two-stage version of the Long March 2E rocket, which in turn was based on the Long March 2C launch vehicle.[2] It is launched from complex SLS at the Jiuquan Satellite Launch Center. The Long March 2F made its maiden flight on 19 November 1999, with the Shenzhou 1 spacecraft. After the flight of Shenzhou 3, CPC General Secretary and President Jiang Zemin named the rocket "Shenjian", meaning "Divine Arrow".[3]

Country of originChina
Height62 m (203 ft)[1]
Quick facts Function, Manufacturer ...
Long March 2F
The Long March 2F rocket with Shenzhou 13 spacecraft mounted on the top
FunctionMedium-lift launch vehicle
ManufacturerChina Academy of Launch Vehicle Technology
Country of originChina
Size
Height62 m (203 ft)[1]
Diameter3.35 m (11.0 ft)[1]
Mass464,000 kg (1,023,000 lb)[1]
Stages2
Capacity
Payload to LEO
Mass8,400 kg (18,500 lb)[1]
Associated rockets
FamilyLong March 2
Launch history
StatusActive
Launch sitesJiuquan Satellite Launch Center
Total launches28
Success(es)28
First flight19 November 1999
Last flight7 February 2026 (most recent)
Carries passengers or cargoShenzhou
Tiangong-1
Tiangong-2
Reusable experimental spacecraft
Boosters
No. boosters4
Height15.3 m (50 ft)
Diameter2.3 m (7 ft 7 in)
Empty mass3,200 kg (7,100 lb)
Gross mass41,000 kg (90,000 lb)
Powered by1 YF-20B per booster
Maximum thrust814 kN (183,000 lbf)
Total thrust3,256 kN (732,000 lbf)
Specific impulse291 s (2.85 km/s)
Burn time128 seconds
PropellantN2O4 / UDMH
First stage
Height23.7 m (78 ft)
Diameter3.4 m (11 ft)
Empty mass9,500 kg (20,900 lb)
Gross mass196,500 kg (433,200 lb)
Powered by4 YF-20B
Maximum thrust3,256 kN (732,000 lbf)
Specific impulse291 s (2.85 km/s)
Burn time166 seconds
PropellantN2O4 / UDMH
Second stage
Height13.5 m (44 ft)
Diameter3.4 m (11 ft)
Empty mass5,500 kg (12,100 lb)
Gross mass91,500 kg (201,700 lb)
Powered by1 YF-24B
Maximum thrust831 kN (187,000 lbf)
Specific impulse289 s (2.83 km/s)
Burn time300 seconds
PropellantN2O4 / UDMH
Close

On 29 December 2002, a Long March 2F launched Shenzhou 4 for a final uncrewed test of the Shenzhou spacecraft for the upcoming flight of the first crewed mission. Until then, all missions were uncrewed.

On 15 October 2003, a Long March 2F launched Shenzhou 5, China's maiden crewed mission and achieved its first human spaceflight. Since then, the rocket has launched twenty more missions into orbit with the latest being the Shenzhou 20 spacecraft.[4][5][6][7]

Differences from the Long March 2E

Externally, the rocket is similar to the Long March 2E from which it was derived. Most of the changes involve the addition of redundant systems to improve safety, although there are some structural modifications that allow the rocket to support the heavier fairing required by the Shenzhou capsule. The rocket is also capable of lifting heavier payloads with the addition of extra boosters to the first stage.[8]

The rocket also has an "advanced fault monitoring and diagnosis system to help the astronauts escape in time of emergency" (in other words, a launch escape system), and is the first Chinese made rocket to be assembled and rolled out to its launch site vertically.[9]

Derivatives

A derivative called Long March 2F/G, first launched in 2011, was made to replace the existing 2F variant. For uncrewed launches, Long March 2F/T was designed, which launched space laboratories such as Tiangong-1 and Tiangong-2. It dispenses with the launch escape system and supports a larger fairing to accommodate the bulkier payloads.[10] For launching payloads like reusable experimental spacecraft, the Long March 2F/G's fairing has bumps added to enclose parts of the payload (such as wingtips) without using a larger fairing.[11][12][13]

Vibration issues

During the Shenzhou 5 flight, Yang Liwei became unwell due to heavy vibrations from the rocket. Although the problem was reduced somewhat by modifications to the rocket, vibrations were reported again in Shenzhou 6 necessitating further changes. According to Jing Muchun, chief designer of the Long March 2F "We made changes to the pipelines of the rocket engine, adjusting its frequency. A new design for the pressure accumulator produced evident results. The vibration has now been reduced by more than 50%".[14] During the launch preparations for the Shenzhou 14 mission chief designer Gao Xu said incremental improvements made to the rocket's design mean vibrations felt by the taikonauts would be similar to that felt in a car driven on a highway.[15]

The predecessor Long March 2E had also been known for vibration. During two launches, excessive vibration caused the collapse of the payload fairing, destroying the Optus B2 and Apstar 2 satellites.[16] After the payload fairing was redesigned, excessive vibration also damaged the AsiaSat 2 satellite during launch. After its successful launch of the Echostar 1 satellite on 28 December 1995 the rocket was officially retired from service.[17]

Launch statistics

1
2
3
1999
2005
2010
2015
2020
2025
  •   Failure
  •   Partial failure
  •   Success
  •   Planned

List of launches

More information Flight number, Serial number ...
Close

See also

References

Related Articles

Wikiwand AI