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Thor DM-21
Part of Thor DM-19 Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1969. Thrust: 760.64 kN (170,999 lbf). Gross mass: 48,354 kg (106,602 lb). Unfuelled mass: 2,948 kg (6,499 lb). Specific impulse: 285 s. Specific impulse sea level: 250 s. Burn time: 164 s. Height: 18.41 m (60.40 ft). Diameter: 2.44 m (8.00 ft). Span: 2.44 m (8.00 ft).

Cost $ : 7.830 million.



Country: USA. Engines: MB-3-1. Launch Vehicles: Thor Delta A, Thor Ablestar, Thor Agena B, Thor Ablestar 2, Thor DSV-2D, Thor Agena D, Thor Delta B, Thor Delta C, Thor Delta C1. Propellants: Lox/Kerosene.

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