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Beal BA-2 Stage 3
H2O2/Kerosene propellant rocket stage. Thrust declines to 50% of initial value at shut down.

Status: Development 2000. Thrust: 196.00 kN (44,062 lbf). Gross mass: 36,700 kg (80,900 lb). Unfuelled mass: 2,855 kg (6,294 lb). Specific impulse: 300 s. Burn time: 600 s. Height: 8.20 m (26.90 ft). Diameter: 6.20 m (20.30 ft). Span: 6.20 m (20.30 ft).



Country: USA. Engines: BA-44. Propellants: H2O2/Kerosene.

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