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Delta Thor TA
Part of Thor DM-19 Family
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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