Propulsion 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) |
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 8048 |
|
|
68.9 |
2707 |
3.055 |
120 |
0.0255 |
8.3 |
B |
Bell 8081 |
70.7 | 2775 | 6.112 | 240 | 0.0255 | 17.0 | ||
B, D |
Bell 8096 |
71.2 | 2854 | 6.112 | 245 | 0.0249 | 17.4 |