|
Propulsion
Titan III & IV
Booster
|
Launcher
|
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
|
|
3C, 3C+, 3D, 3E
|
UA-1205
|
max |
5,293.4 |
2334 |
max |
5,849.5 |
2579 |
192.45 |
110.8 |
max |
2.2680 |
496.36 |
|
ave |
4,053.7 |
ave |
4,479.4 |
ave |
1.7368 |
|
34D, III
|
UA-1206
|
max |
5,615.9 |
2354 |
max |
6,200.7 |
2599 |
210.80 |
120.7 |
max |
2.3861 |
547.78 |
|
ave |
4,110.2 |
ave |
4,538.8 |
ave |
1.7464 |
|
34D7, IVA
|
UA-1207
|
max |
6,458.2 |
2403 |
max |
7,117.2 |
2648 |
268.30 |
128.9 |
max |
2.6880 |
710.39 |
|
ave |
5,001.0 |
ave |
5,511.4 |
ave |
2.0815 |
|
IVB
|
SRMU
|
max |
6,407.7 |
2465 |
max |
7,565.0 |
2757 |
315.45 |
135.7 |
max |
2.7443 |
869.53 |
|
ave |
5,730.7 |
ave |
6,765.8 |
ave |
2.3245 |
|
LR-87-AJ-9
|
LR-87-AJ-11(A)
|
Stage 1
|
Launcher
|
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
|
|
3A, 3B, 3C
|
LR-87-AJ-9
(2)
|
1,941.7
|
2473
|
2,339.8
|
2980
|
117.76
|
150
|
0.7851
|
351.0
|
|
3B+, 3C+, 3D, 3E
|
LR-87-AJ-11 (2)
|
2,001.7 |
2472 |
2,413.2 |
2980 |
118.21 |
146 |
0.8097 |
352.3 |
|
3BS, 34D
|
LR-87-AJ-11 (2)
|
2,001.7 |
2472 |
2,413.2 |
2980 |
131.98 |
163 |
0.8097 |
393.3 |
|
III
|
LR-87-AJ-11 (2)
|
2,001.7 |
2472 |
2,413.2 |
2980 |
131.98 |
163 |
0.8097 |
393.3 |
|
34D7, IVA
|
LR-87-AJ-11A (2)
|
2,034.6 |
2473 |
2,451.9 |
2980 |
152.57 |
185.5 |
0.8227 |
454.7 |
|
IVB
|
LR-87-AJ-11A (2)
|
2,039.5 |
2473 |
2,457.7 |
2980 |
152.57 |
185 |
0.8247 |
454.7 |
|
LR-91-AJ-9
|
LR-91-AJ-11(A)
|
Stage 2
|
Launcher
|
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
|
|
3A, 3B, 3C
|
LR-91-AJ-9
|
|
|
453.7 |
3094 |
30.48 |
208 |
0.1466 |
94.3 |
|
3B+, 3C+, 3D, 3E
|
LR-91-AJ-11
|
|
|
460.4 |
3094 |
30.48 |
205 |
0.1488 |
94.3 |
|
3BS, 34D
|
LR-91-AJ-11
|
|
|
460.4 |
3094 |
30.48 |
205 |
0.1488 |
94.3 |
|
III
|
LR-91-AJ-11
|
|
|
460.4 |
3094 |
30.48 |
205 |
0.1488 |
94.3 |
|
34D7, IVA
|
LR-91-AJ-11A
|
|
|
467.1 |
3094 |
34.74 |
230 |
0.1510 |
107.5 |
|
IVB
|
LR-91-AJ-11A
|
|
|
472.2 |
3094 |
34.74 |
227.5 |
0.1526 |
107.5 |
|
RL-10A-3-3AT (Centaur-T)
|
AJ-10-138 (Transtage)
|
|
I.U.S.
|
Orbus-6
|
Orbus-21
|
Stage 3
|
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
|
|
Centaur D-1T
|
RL-10A-3-3T
|
|
|
133.4 |
4336 |
13.790 |
448.2 |
0.0308 |
59.8 |
|
Centaur-T
|
RL-10A-3-3AT
|
|
|
146.8 |
4358 |
20.865 |
619.5 |
0.0337 |
90.9 |
|
RL-10A-4-1
|
|
|
195.7 |
4378 |
20.865 |
466.7 |
0.0447 |
91.3 |
|
Agena D
|
Bell 8096
|
|
|
71.2 |
2854 |
6.112 |
245 |
0.0249 |
17.4 |
|
Agena D+
|
Bell 8096-39
|
|
|
75.3 |
2942 |
6.143 |
240 |
0.0256 |
18.1 |
|
Ascent Agena
|
Bell 8247
|
|
|
71.7 |
2873 |
6.112 |
245 |
0.0249 |
17.6 |
|
Transtage
|
AJ-10-138
|
|
|
71.7 |
3050 |
10.35 |
440 |
0.0235 |
31.6 |
|
I.U.S.
|
ORBUS-21
|
|
|
183.7 |
2898 |
9.759 |
154 |
0.0634 |
28.3 |
|
ORBUS-6E
|
|
|
79.2 |
2976 |
2.735 |
103 |
0.0266 |
8.1 |
|
T.O.S.
|
ORBUS-21H
|
|
|
193.3 |
2883 |
9.779 |
146 |
0.0670 |
28.2 |
|
-
|
ORBUS-21S
|
|
|
199.5 |
2883 |
9.550 |
138 |
0.0692 |
27.5 |
|
-
|
ORBUS-7S
|
|
|
153.5 |
2764 |
3.330 |
60 |
0.0555 |
9.2 |
|
Star 63F
|
TE-M-963-2
|
|
|
104.62 |
2938 |
4.264 |
119.8 |
0.0356 |
12.53 |
|
