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Delta Thor RS27
Part of Thor DM-19
LOx/Kerosene propellant rocket stage. .

AKA: Extended Length Thor RS-27. Status: Retired 1989. Thrust: 1,030.22 kN (231,602 lbf). Gross mass: 84,368 kg (185,999 lb). Unfuelled mass: 4,360 kg (9,610 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 223 s. Height: 22.37 m (73.39 ft). Diameter: 2.44 m (8.00 ft). Span: 2.44 m (8.00 ft).

Cost $ : 11.600 million.



Country: USA. Engines: RS-27. Launch Vehicles: Delta 2914, Delta 3914, Delta 3910, Delta 3910/PAM, Delta 3913, Delta 3920, Delta 3920/PAM, Delta 3924, Delta 5000, Delta 3920-8, Delta 5920-8. Propellants: Lox/Kerosene.

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