The Long March 2F rocket withShenzhou 13 spacecraft mounted on the top | |
| Function | Medium-lift launch vehicle |
|---|---|
| Manufacturer | China Academy of Launch Vehicle Technology |
| Country of origin | China |
| Size | |
| Height | 62 m (203 ft)[1] |
| Diameter | 3.35 m (11.0 ft)[1] |
| Mass | 464,000 kg (1,023,000 lb)[1] |
| Stages | 2 |
| Capacity | |
| Payload toLEO | |
| Mass | 8,400 kg (18,500 lb)[1] |
| Associated rockets | |
| Family | Long March 2 |
| Launch history | |
| Status | Active |
| Launch sites | Jiuquan Satellite Launch Center |
| Total launches | 27 |
| Success(es) | 27 |
| First flight | 19 November 1999 |
| Last flight | 25 November 2025(most recent) |
| Carries passengers or cargo | Shenzhou Tiangong-1 Tiangong-2 Reusable experimental spacecraft |
| Boosters | |
| No. boosters | 4 |
| Height | 15.3 m (50 ft) |
| Diameter | 2.3 m (7 ft 7 in) |
| Empty mass | 3,200 kg (7,100 lb) |
| Gross mass | 41,000 kg (90,000 lb) |
| Powered by | 1YF-20B per booster |
| Maximum thrust | 814 kN (183,000 lbf) |
| Total thrust | 3,256 kN (732,000 lbf) |
| Specific impulse | 291 s (2.85 km/s) |
| Burn time | 128 seconds |
| Propellant | N2O4 /UDMH |
| First stage | |
| Height | 23.7 m (78 ft) |
| Diameter | 3.4 m (11 ft) |
| Empty mass | 9,500 kg (20,900 lb) |
| Gross mass | 196,500 kg (433,200 lb) |
| Powered by | 4YF-20B |
| Maximum thrust | 3,256 kN (732,000 lbf) |
| Specific impulse | 291 s (2.85 km/s) |
| Burn time | 166 seconds |
| Propellant | N2O4 /UDMH |
| Second stage | |
| Height | 13.5 m (44 ft) |
| Diameter | 3.4 m (11 ft) |
| Empty mass | 5,500 kg (12,100 lb) |
| Gross mass | 91,500 kg (201,700 lb) |
| Powered by | 1YF-24B |
| Maximum thrust | 831 kN (187,000 lbf) |
| Specific impulse | 289 s (2.83 km/s) |
| Burn time | 300 seconds |
| Propellant | N2O4 /UDMH |
TheLong March 2F (Chinese:长征二号F火箭Changzheng 2F), also known as theCZ-2F,LM-2F andShenjian (神箭, "Divine Arrow"),[1] is a Chineseorbitalcarrier rocket, part of theLong March 2 rocket family. Designed to launchcrewedShenzhou spacecraft, the Long March 2F is ahuman-rated two-stage version of theLong March 2E rocket, which in turn was based on theLong March 2C launch vehicle.[2] It is launched from complex SLS at theJiuquan Satellite Launch Center. The Long March 2F made its maiden flight on 19 November 1999, with theShenzhou 1 spacecraft. After the flight ofShenzhou 3, CPC General Secretary and PresidentJiang Zemin named the rocket "Shenjian", meaning "Divine Arrow".[3]
On 29 December 2002, a Long March 2F launchedShenzhou 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 launchedShenzhou 5, China's maiden crewed mission and achieved its firsthuman spaceflight. Since then, the rocket has launched twenty more missions into orbit with the latest being theShenzhou 20 spacecraft.[4][5][6][7]
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, alaunch escape system), and is the first Chinese made rocket to be assembled and rolled out to its launch site vertically.[9]
A derivative calledLong 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 asTiangong-1 andTiangong-2. It dispenses with the launch escape system and supports a larger fairing to accommodate the bulkier payloads.[10] For launching payloads likereusable 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]
During theShenzhou 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 inShenzhou 6 necessitating further changes. According toJing 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 theShenzhou 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 predecessorLong March 2E had also been known for vibration. During two launches, excessive vibration caused the collapse of the payload fairing, destroying theOptus B2 andApstar 2 satellites.[16] After the payload fairing was redesigned, excessive vibration also damaged theAsiaSat 2 satellite during launch. After its successful launch of theEchostar 1 satellite on 28 December 1995 the rocket was officially retired from service.[17]
| Flight number | Serial number | Date (UTC) | Version | Launch site | Payload | Orbit | Crew | Result | Remarks |
|---|---|---|---|---|---|---|---|---|---|
| 1 | Y1 | 19 November 1999 22:30 | 2F | LA-4/SLS-1,JSLC | Shenzhou 1 | LEO | N/A | Success | First uncrewed test of theShenzhou spacecraft |
| 2 | Y2 | 9 January 2001 17:00 | 2F | LA-4/SLS-1, JSLC | Shenzhou 2 | LEO | N/A | Success | Second uncrewed test of the Shenzhou spacecraft, carried live animals. |
| 3 | Y3 | 25 March 2002 14:15 | 2F | LA-4/SLS-1, JSLC | Shenzhou 3 | LEO | N/A | Success | Third uncrewed test of the Shenzhou spacecraft. |
| 4 | Y4 | 29 December 2002 16:40 | 2F | LA-4/SLS-1, JSLC | Shenzhou 4 | LEO | N/A | Success | Final uncrewed test of the Shenzhou spacecraft prior to flying with crew. |
| 5 | Y5 | 15 October 2003 01:00 | 2F | LA-4/SLS-1, JSLC | Shenzhou 5 | LEO | Success | China's first crewed spaceflight. | |
| 6 | Y6 | 12 October 2005 01:00 | 2F | LA-4/SLS-1, JSLC | Shenzhou 6 | LEO | Success | Second crewed spaceflight, first with two astronauts. | |
| 7 | Y7 | 25 September 2008 13:10 | 2F | LA-4/SLS-1, JSLC | Shenzhou 7 | LEO | Success | First flight with three crew members, first to featureextravehicular activity. | |
| 8 | T1 | 29 September 2011 13:16 | 2F/T | LA-4/SLS-1, JSLC | Tiangong 1 | LEO | N/A | Success | The first Chinese space station. Modified version Long March 2F/G with larger payload fairing.[10] |
| 9 | Y8 | 31 October 2011 21:58 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 8 | LEO | N/A | Success | Uncrewed spaceflight to test automaticrendezvous anddocking withTiangong-1 |
| 10 | Y9 | 16 June 2012 10:37 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 9 | LEO | Success | Three crew members, to test rendezvous and docking with Tiangong-1. | |
| 11 | Y10 | 11 June 2013 09:38 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 10 | LEO | Success | Three crew members; rendezvous and docking with Tiangong-1. | |
| 12 | T2 | 15 September 2016 14:04 | 2F/T | LA-4/SLS-1, JSLC | Tiangong 2 | LEO | N/A | Success | Second Chinese space laboratoryTiangong-2, launched by 2F/G variant. |
| 13 | Y11 | 16 October 2016 23:30 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 11 | LEO | Success | Two crew members;[18] rendezvous and docking with Tiangong-2 for a 30-day mission. | |
| 14 | T3 | 4 September 2020 07:30 | 2F/T | LA-4/SLS-1, JSLC | Reusable Experimental Spacecraft[19] | LEO | N/A | Success | Test flight of a reusable experimental spacecraft.[19][20] |
| 15 | Y12 | 17 June 2021 01:22 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 12 | LEO | Success | Three crew members; first visit toTianhe, the first module of theChinese Space Station, for a three-month mission. | |
| 16 | Y13 | 15 October 2021 16:23 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 13 | LEO | Success | Three crew members; visitedTianhe to continue construction of the space station for a six-month mission.[21] | |
| 17 | Y14 | 5 June 2022 02:44 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 14 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission.[22] | |
| 18 | T4 | 4 August 2022 16:00 | 2F/T | LA-4/SLS-1, JSLC | Reusable Experimental Spacecraft | LEO | N/A | Success | Second test flight of a reusable experimental spacecraft.[23][24] |
| 19 | Y15 | 29 November 2022 15:08 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 15 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission.[25] | |
| 20 | Y16 | 30 May 2023 01:31 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 16 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 21 | Y17 | 26 October 2023 03:13 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 17 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 22 | T5 | 14 December 2023 14:12 | 2F/T | LA-4/SLS-1, JSLC | Reusable Experimental Spacecraft | LEO | N/A | Success | Third test flight of a reusable experimental spacecraft.[26] |
| 23 | Y18 | 25 April 2024 12:59 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 18 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 24 | Y19 | 29 October 2024 20:27 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 19 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 25 | Y20 | 24 April 2025 09:17 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 20 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 26 | Y21 | 31 October 2025 15:44 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 21 | LEO | Success | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 27 | Y22 | 25 November 2025 04:11 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 22 | LEO | N/A | Success | Replacement Spacecraft for returnShenzhou 21 crew. |
| 28 | T6 | 2025 | 2F/T | LA-4/SLS-1, JSLC | Reusable Experimental Spacecraft | LEO | N/A | Planned | |
| 29 | Y23 | April 2026 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 23 | LEO | Planned | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 30 | Y24 | October 2026 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 24 | LEO | Planned | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 31 | Y25 | April 2027 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 25 | LEO | Planned | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. | |
| 32 | Y26 | October 2027 | 2F/G | LA-4/SLS-1, JSLC | Shenzhou 26 | LEO | Planned | Three crew members; rendezvous and docking with the Chinese space station for a six-month mission. |
The principal difference between the Shenzhou-launching Long March 2F and its 2F/G cousin is easy to spot. The 2F/G carries a very different payload fairing at its top. This accounts. for the larger dimensions of the Tiangong laboratory, which wouldn't fit inside the standard payload fairing for the 2F.
It also lacks an emergency escape system. With no astronauts on board, the escape rocket and stabilizer panels that help Shenzhou spacecraft to separate from their rocket in a launch failure are not needed. This simplifies the design and also reduces the weight of the rocket. That's critical. Tiangong modules weigh more than Shenzhou spacecraft, so this helps to keep the overall launch mass within performance limits.