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Long March 7 information


Long March 7
Long March 7 Y6 transporting to launch site
FunctionMedium to heavy
launch vehicle
ManufacturerCALT
Country of originChina
Size
Height
  • CZ-7: 53.10 m (174.2 ft)
  • CZ-7A: 60.13 m (197.3 ft) [1]
Diameter3.35 m (11.0 ft)
Mass
  • CZ-7: 597,000 kg (1,316,000 lb) [2]
  • CZ-7A: 573,000 kg (1,263,000 lb) [1]
Stages
  • CZ-7: Two
  • CZ-7A: Three [3]
Capacity
Payload to LEO (200 x 400 km x 42°)
Mass13,500 kg (29,800 lb)
Payload to GTO
Mass7,000 kg (15,000 lb) [3]
Payload to TLI
Mass5,000 kg (11,000 lb)
Payload to SSO
Altitude700 km (430 mi)
Mass5,500 kg (12,100 lb)
Associated rockets
FamilyLong March
ComparableDelta IV, Atlas V, Falcon 9 Block 5, GSLV Mk.III, H-IIA
Launch history
StatusActive
Launch sitesWenchang, LC-2
Total launches14 (7:8, 7A:6)
Success(es)13 (7:8, 7A:5)
Failure(s)1 (7:0, 7A:1)
First flight
  • Long March 7: 25 June 2016
  • Long March 7A: 16 march 2020
Last flight
  • Long March 7: 17 January 2024
  • Long March 7A: 3 November 2023
    (Both Active)
Boosters – K2 booster
No. boosters4
Height27 m (89 ft)
Diameter2.25 m (7 ft 5 in)
Powered by1 YF-100
Maximum thrustSL: 1,200 kN (270,000 lbf)
Vac: 1,340 kN (300,000 lbf)
Total thrustSL: 4,800 kN (1,100,000 lbf)
Vac: 5,360 kN (1,200,000 lbf)
Specific impulseSL: 300 s (2.9 km/s)
Vac: 335 s (3.29 km/s)
PropellantRP-1 / LOX
First stage – K3 core module
Diameter3.35 m (11.0 ft)
Powered by2 YF-100
Maximum thrustSea level: 2,400 kN (540,000 lbf)
Vacuum: 2,680 kN (600,000 lbf)
Specific impulseSea level: 300 s (2.9 km/s)
Vacuum: 335 s (3.29 km/s)
PropellantRP-1 / LOX
Second stage
Diameter3.35 m (11.0 ft)
Powered by4 YF-115
Maximum thrust706 kN (159,000 lbf)
Specific impulse342 s (3.35 km/s)
PropellantRP-1 / LOX
Third stage (CZ-7A)
Diameter3.0 m (9.8 ft)
Empty mass2,800 kg (6,200 lb)
Gross mass21,000 kg (46,000 lb)
Propellant mass18,200 kg (40,100 lb)
Powered by2 YF-75
Maximum thrust167.17 kN (37,580 lbf)
Specific impulse4,295 m/s (438.0 s)
Burn time478 seconds
PropellantLH2 / LOX
Fourth stage (optional) – YZ-1A
Powered by1 × YF-50D
Maximum thrust6.5 kN (1,500 lbf)
Specific impulse315.5 s (3.094 km/s)
PropellantN2O4 / UDMH

The Long March 7 (Chinese: 长征七号运载火箭), or Chang Zheng 7 in pinyin, abbreviated LM-7 for export or CZ-7 within China, originally Long March 2F/H or Chang Zheng 2F/H, nicknamed Bingjian (冰箭; 'the Ice Arrow'), is a Chinese liquid-fuelled launch vehicle of the Long March family, developed by the China Aerospace Science and Technology Corporation (CAST).[4] It made its inaugural flight on 25 June 2016.

Designed as a replacement of the Long March 2F, Long March 7 and its variants was expected to be the workhorse of the fleet, projected to account for around 70% of all Chinese launches. Long March 7 plays a critical role in the Chinese Space Station program: it is used to launch the Tianzhou robotic cargo and resupply spacecraft to the station. The rocket was intended to replace the Long March 2F as China's crew-rated launch vehicle in the future,[4] although by 2023 this role has apparently been taken over by the under-development Long March 10 and Long March 10A.

Since 2020, in addition to the base Long March 7 configuration, there is the Long March 7A (CZ-7A etc.) variant which differs from the base CZ-7 by the addition of a liquid hydrogen-liquid oxygen third stage inherited from the third stage of the Long March 3B.[3] The rocket has also been developed into the Long March 8.

  1. ^ a b Jones, Andrew (16 February 2020). "China quietly rolls out new rocket to launch mystery satellite". SpaceNews. Retrieved 16 February 2020.
  2. ^ [1] - 8 May 2020
  3. ^ a b c Jones, Andrew (14 February 2020). "China prepares to launch new rockets as part of push to boost space program". SPACE.com. Retrieved 14 February 2020.
  4. ^ a b Cite error: The named reference guokr-20160303 was invoked but never defined (see the help page).

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