|
|
|
Propulsion Delta
|
|
|
Booster
|
Versions |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Combustion |
Total Imp |
|||
| kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s | |||||
|
D, E, E1, G, J |
Castor I (TX-33-52) |
max | 168.6 | 1655 | max | 246.4 | 2420 | 3.327 | 37 | max | 0.1019 | 8.05 |
| min | 148.8 | min | 217.6 | min | 0.0899 | |||||||
|
L, M, N etc. |
Castor II (TX-354) |
max | 189.1 | 1692 | max | 274.9 | 2460 | 3.728 | 40 | max | 0.1118 | 9.17 |
| min | 157.7 | min | 229.2 | min | 0.0932 | |||||||
Stage 1
|
Versions |
Engines |
Tank |
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 | |||
|
Thor-Delta |
MB-3-I |
DSV |
667.2 | 2456 | 756.2 | 2784 | 45.40 | 164.4 | 0.2717 | 126.2 |
|
A, B, C, C1 |
MB-3-II |
DSV | 734.0 | 2456 | 831.8 | 2784 | 46.64 | 153.8 | 0.2988 | 129.6 |
|
D, E, E1, G, J |
MB-3-III |
DSV | 756.2 | 2456 | 858.5 | 2784 | 46.64 | 149.3 | 0.3080 | 129.8 |
|
L, M, N, 0000 |
MB-3-III |
LTT | 756.2 | 2456 | 858.5 | 2784 | 67.81 | 217.0 | 0.3080 | 188.7 |
|
1000 |
MB-3-III |
ELLT | 756.2 | 2456 | 858.5 | 2784 | 81.42 | 260.5 | 0.3080 | 226.5 |
|
all versions |
2 Verniers LR-101 |
8.9 | 1952 | 11.1 | 2442 | 0.0046 | ||||
Stage 2
|
Versions |
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 | ||
|
Thor-Delta |
AJ-10-142 |
33.4 | 2648 | 1.575 | 125 | 0.0126 | 4.17 | ||
|
A |
AJ-10-118 |
33.4 | 2648 | 1.575 | 125 | 0.0126 | 4.17 | ||
|
B, C, C1, D |
AJ-10-118D |
33.7 | 2672 | 2.140 | 169.7 | 0.0126 | 5.72 | ||
|
E, E1, G, J, L, M, N |
AJ-10-118E |
35.2 | 2726 | 4.862 | 377 | 0.0129 | 13.2 | ||
|
Delta 0000, 1000 |
AJ-10-118F |
42.3 | 3089 | 4.586 | 334.9 | 0.0137 | 14.2 |
Stage 3
|
Versions |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Combustion |
Total Imp |
|
kN |
N*s/kg |
kN |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
|
Thor-Delta, A, B |
X-248 |
|
|
13.8 |
2785 |
0.211 |
42.6 |
0.0049 |
0.59 |
|
C, D, E |
X-258 |
24.8 | 2785 | 0.235 | 26.4 | 0.0089 | 0.65 | ||
|
C1, E1, L |
FW-4D |
26.4 | 2805 | 0.274 | 29.2 | 0.0094 | 0.77 | ||
|
J, M, N |
Star-37D (TE-M-364-3) |
42.3 | 2846 | 0.653 | 44.0 | 0.0149 | 1.86 | ||
|
1604 |
Star-37E (TE-M-364-4) |
66.7 | 2802 | 1.039 | 43.6 | 0.0238 | 2.91 |
Stage 4
|
Versions |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Combustion |
Total Imp |
| kN | N*s/kg | kN | N*s/kg | tons | s | t/s | MN*s | ||
|
D, C |
X-258 |
24.8 | 2785 | 0.235 | 26.4 | 0.0089 | 0.65 |
