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Delta Thor TA
Part of Thor DM-19
LOx/Kerosene propellant rocket stage. .
AKA: Thrust Augmented Thor. Status: Retired 1968. Thrust: 866.71 kN (194,844 lbf). Gross mass: 49,442 kg (109,000 lb). Unfuelled mass: 3,175 kg (6,999 lb). Specific impulse: 290 s. Specific impulse sea level: 256 s. Burn time: 150 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-3-3.
Launch Vehicles:
Thor SLV-2A Agena D,
Thor SLV-2A Agena B,
Thor Delta D,
Thor Delta E,
Thor Delta E1,
Thor Delta G,
Thor Delta J.
Propellants:
Lox/Kerosene.
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