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Thor DM-21
Part of Thor DM-19
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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