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Thor DM-19
Status: Retired 1980. Thrust: 758.71 kN (170,565 lbf). Gross mass: 49,340 kg (108,770 lb). Unfuelled mass: 3,125 kg (6,889 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 165 s. Height: 18.42 m (60.43 ft). Diameter: 2.44 m (8.00 ft). Span: 2.44 m (8.00 ft).
Cost $ : 4.930 million.
| Thor DM-21 LOx/Kerosene propellant rocket stage. . |
| Delta Thor TA LOx/Kerosene propellant rocket stage. . |
| Delta Thor LT LOx/Kerosene propellant rocket stage. . |
| Delta Thor XLT-C LOx/Kerosene propellant rocket stage. . |
| Delta Thor RS27 LOx/Kerosene propellant rocket stage. . |
| Delta Thor ELT LOx/Kerosene propellant rocket stage. . |
| Delta Thor XLT LOx/Kerosene propellant rocket stage. . |
| H-1-1 LOx/Kerosene propellant rocket stage. License built MB-3 ELT Thor. |
| H-2-1 LOx/LH2 propellant rocket stage. . |
| Delta 3 - 1 LOx/Kerosene propellant rocket stage. The first stage of the Delta III is powered by a Rocketdyne RS-27A main engine which has a 12:1 expansion ratio and employs a turbine/turbopump, a regeneratively cooled thrust chamber and nozzle, and a hydraulically gimbaled thrust chamber and nozzle that provides pitch and yaw control. |
| H-2A-1 LOx/LH2 propellant rocket stage. Lower cost version of H-2 first stage. Can be throttled to 72% thrust. |
| H-2A LRB LOx/LH2 propellant rocket stage. Two-engine version of H-2A-1 used as strap-on booster. |
Country: USA. Engines: LR79-7. Launch Vehicles: Thor DM-18, Thor Able, Thor Able I, Thor DM-18A, Thor Agena A, Thor Able II, Thor Able III, Thor Able II M1, Thor DM-18C, Thor Able IV, Thor Delta, Thor DSV-2E, Thor SLV-2 Agena D, Thor DSV-2F, Thor SLV-2 Agena B, Thor DSV-2J, Thor DSV-2G, Thor MG-18, Thor Burner 1, Thor Burner 2, Thor Burner 2A, Thor DSV-2U. Propellants: Lox/Kerosene.
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