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Diamant-2
Part of Topaze Family
N2O4/UDMH propellant rocket stage. .

AKA: Topaze. Status: Out of production. Thrust: 120.08 kN (26,996 lbf). Gross mass: 2,815 kg (6,206 lb). Unfuelled mass: 540 kg (1,190 lb). Specific impulse: 255 s. Specific impulse sea level: 225 s. Burn time: 39 s. Height: 4.57 m (14.99 ft). Diameter: 0.80 m (2.62 ft). Span: 0.80 m (2.62 ft).

Cost $ : 0.700 million.



Country: France. Engines: Topaze. Launch Vehicles: Saphir VE231, Diamant A. Propellants: N2O4/UDMH.

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