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Pegasus Tanks
xLOx/LH2 propellant rocket drop tank. . Four tanks jettisoned at 130 seconds after liftoff; two at 250 seconds, last two at orbital insertion, 360 seconds after liftoff.

Status: Study 1966. Gross mass: 20,000 kg (44,000 lb). Unfuelled mass: 3,700 kg (8,100 lb). Specific impulse: 459 s. Specific impulse sea level: 359 s. Burn time: 130 s. Height: 18.90 m (62.00 ft). Diameter: 4.57 m (14.99 ft). Span: 4.57 m (14.99 ft).

Cost $ : 6.000 million. No Engines: 0.

Country: USA. Engines: None. Launch Vehicles: Pegasus VTOVL. Propellants: Lox/LH2.
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