*Stages: 3
- Length 28.220 m
- Wingspan 3.810 m
- Liftoff mass 81,075 kg
- Liftoff thrust 1101.2 kN
- Thrust-to-mass 13.6 N/kg
- Payload
- 930 kg (rotating)
- 750 kg(non-rotating)
(300 km circular, inclination 57 deg)
- Orbit insertion accuracy
- diff of ecc 0.001 to 0.005
- diff of inc < 0.3 degrees
(300～1000 km circular orbit)
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- Length 19.735 m
- Diameter 2.250 m
- Mass of the stage 65,040 kg
- Mass of the structure 4,080 kg
- Mass of the fuel 60,860 kg
- Booster YF-2A
- Fuel HNO3-27S/UDMH
- Liftoff thrust (sealevel) 1101.2 kN
- Specific impulse: 2378 N·s/kg
- Burn time ~132 s
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- Length 6.037 m
- Diameter 2.250 m
- Stage mass 13,490 kg
- Structure mass 1,100 kg
- Fuel mass 12,380 kg
- Booster YF-40 (two boosters)
- Fuel N2O4/UDMH
- Thrust in vacuum 100.86 kN
- Specific impulse 2981.2 N·s/kg
- Burn time 360 s
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- Length: 1.696 m
- Diameter: 2.054 m
- Stage mass 1,315 kg
- Structure mass 523 kg
- Fuel mass 792 kg
- liquid 147 kg
- solid 645 kg
- Solid rocket booster: FG-36
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