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CZ-NGLV-300
LOx/Kerosene propellant rocket stage. From top to bottom the 3.35-m Chinese new generation launch vehicle consists of a 90.7 cubic meter liquid oxygen tank, an intertank section, a 47.7 cubic meter kerosene tank, and an engine section with two gimbaled LOX /Kerosene engines of 1200 kN vacuum thrust each. The oxygen tank is pressurized using oxygen bled from the engine and helium is used to pressurize the kerosene tank. The engines can be throttled to 65% of rated thrust. Burn time shown assumes full thrust during engine burn.

Status: In development. Thrust: 2,680.35 kN (602,567 lbf). Gross mass: 147,000 kg (324,000 lb). Unfuelled mass: 12,000 kg (26,000 lb). Specific impulse: 336 s. Specific impulse sea level: 301 s. Burn time: 160 s. Height: 26.30 m (86.20 ft). Diameter: 3.35 m (10.99 ft). Span: 4.60 m (15.00 ft).

No Engines: 2.



Country: China. Engines: YF-120t. Launch Vehicles: CZ-NGLV-320, CZ-NGLV-522, CZ-NGLV-522/HO, CZ-NGLV-504, CZ-NGLV-504/HO. Propellants: Lox/Kerosene.

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