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GSLV-3 stage
Part of N1 Block R Family
LOx/LH2 propellant rocket stage. The stage finally reached hardware status as a joint Russian-Indian development for India's GSLV booster.

AKA: Geostationary Satellite Launch Vehicle. Status: Active. Thrust: 75.05 kN (16,872 lbf). Gross mass: 14,600 kg (32,100 lb). Unfuelled mass: 2,200 kg (4,800 lb). Specific impulse: 460 s. Burn time: 675 s. Height: 8.72 m (28.60 ft). Diameter: 2.80 m (9.10 ft). Span: 2.80 m (9.10 ft).



Country: India. Engines: RD-56M. Launch Vehicles: GSLV. Propellants: Lox/LH2.

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