Engines Thor & Thor-Agena
Booster
|
Version |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| TAT | Castor I (TX-33-39) | 149.1 | 1658 | 217.6 | 2420 | 3.327 | 37 | 0.0899 | 8.05 |
|
Thorad |
Castor II (TX-354) | 157.7 | 1701 | 229.2 | 2472 | 3.728 | 40.2 | 0.0927 | 9.22 |
MB-3-I
Thor Able, Thor-Delta, Thor-Agena
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| 1 | LR-79-NA-9 | 667.2 | 2456 | 756.2 | 2784 | 45.40 | 164.4 | 0.2717 | 126.2 |
|
+ LR-101 (2) |
8.9 | 1952 | 11.1 | 2442 | 0.0046 |
|
MB-3-II
Thor AbleStar, Thor Agena
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| 1 | LR-79-NA-11 | 734.0 | 2456 | 831.8 | 2784 | 46.64 | 153.8 | 0.2988 | 129.6 |
|
+ LR-101 (2) |
8.9 | 1952 | 11.1 | 2442 | 0.0046 |
|
MB-3-III
TAT Agena
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| 1 | LR-79-NA-13 | 756.2 | 2456 | 858.5 | 2784 | 46.64 | 149.3 | 0.3080 | 129.8 |
|
+ LR-101(2) |
8.9 | 1952 | 11.1 | 2442 | 0.0046 |
|
Thorad Agena
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
|
1 |
LR-79-NA-13 | 756.2 | 2456 | 858.5 | 2784 | 67.81 | 217 | 0.3080 | 188.7 |
|
+ LR-101 (2) |
8.9 | 1952 | 11.1 | 2442 | 0.0046 |
|
Able I & II
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| 2 | AJ-10-42 | 33.0 | 2618 | 1.575 | 125 | 0.0126 | 4.12 | ||
| 2 | AJ-10-101A | 33.4 | 2648 | 1.575 | 125 | 0.0126 | 4.17 |
Delta
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| 2 | AJ-10-142 | 33.4 | 2648 | 1.575 | 125 | 0.0126 | 4.17 |
Able Star
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| 2 | AJ-10-104 (D) | 35.2 | 2726 | 4.862 | 377 | 0.0129 | 13.25 |
Agena
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s |
| A | Bell LR 81-BA 5 | 68.9 | 2844 | 2.905 | 120 | 0.0242 | 8.3 | ||
| B | Bell LR 81-BA-7 | 71.2 | 2844 | 5.932 | 237 | 0.0250 | 16.9 | ||
| D | Bell LR 81-BA-9 | 75.6 | 2942 | 6.821 | 265 | 0.0257 | 20.1 |