AKA: CZ H-18;H-18. Status: Development ended 1997. Thrust: 156.00 kN (35,070 lbf). Gross mass: 21,000 kg (46,000 lb). Unfuelled mass: 2,800 kg (6,100 lb). Specific impulse: 440 s. Burn time: 470 s. Height: 12.38 m (40.60 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).
Cost $ : 16.000 million. No Engines: 2.