Propulsion Atlas & Atlas-Agena
MA-1
Atlas B (Score)
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 |
0 |
LR-89-NA-3 (2)
|
1,316.7 |
2432 |
1,497.3 |
2765 |
68.60 |
126.7 |
0.5414 |
189.7 |
1 |
LR-105-NA-3
|
244.7 |
2108 |
353.2 |
3030 |
29.40 |
242.6 |
0.1166 |
85.7 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
245 |
0.0046
|
2.7
|
MA-2
Atlas D-Able
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 |
0 |
LR-89-NA-5 (2)
|
1,334.5 |
2432 |
1,517.4 |
2765 |
74.17 |
135.2 |
0.5487 |
205.2 |
1 |
LR-105-NA-5
|
253.1 |
2108 |
366.1 |
3050 |
36.53 |
293.1 |
0.1200 |
107.3 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
295
|
0.0046
|
3.3
|
Atlas D (OV, Mercury)
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 |
0 |
LR-89-NA-5 (2)
|
1,334.5 |
2432 |
1,517.4 |
2765 |
71.70 |
130.7 |
0.5487 |
198.3 |
1 |
LR-105-NA-5
|
253.1 |
2108 |
366.1 |
3050 |
38.60 |
310 |
0.1200 |
113.5 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
310
|
0.0046
|
3.4
|
Atlas LV-3 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 |
0 |
LR-89-NA-5 (2)
|
1,334.5 |
2432 |
1,517.4 |
2765 |
74.59 |
135.9 |
0.5487 |
206.2 |
1 |
LR-105-NA-5
|
253.1 |
2108 |
366.1 |
3050 |
40.17 |
322.6 |
0.1200 |
118.1 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
325
|
0.0046
|
3.6
|
MA-3
Atlas E/F
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 |
0 |
LR-89-NA-6 (2)
|
1,467.9 |
2510 |
1,662.8 |
2844 |
71.13 |
121.6 |
0.5847 |
202.3 |
1 |
LR-105-NA-6
|
253.1 |
2108 |
366.1 |
3050 |
41.77 |
335.4 |
0.1200 |
122.7 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
335
|
0.0046
|
3.7
|
Atlas SLV-3 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 |
0 |
LR-89-NA-6 (2)
|
1,467.9 |
2510 |
1,662.8 |
2844 |
73.50 |
125.7 |
0.5847 |
209.0 |
1 |
LR-105-NA-6
|
253.1 |
2108 |
366.1 |
3050 |
41.34 |
331.5 |
0.1200 |
121.4 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
335 |
0.0046
|
3.8
|
MA-5
Atlas SLV-3A 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 |
0 |
LR-89-NA-7 (2)
|
1,645.9 |
2530 |
1,863.4 |
2865 |
113.39 |
174.3 |
0.6505 |
324.8 |
1 |
LR-105-NA-7
|
268.7 |
2161 |
385.2 |
3099 |
24.89 |
193 |
0.1243 |
74.3 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
|
195
|
0.0046
|
2.2
|
Atlas H (SLV-3B)
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 |
0 |
LR-89-NA-7 (2)
|
1,679.2 |
2541 |
1,901.6 |
2877 |
91.19 |
138 |
0.6609 |
262.4 |
1 |
LR-105-NA-7
|
269.1 |
2157 |
386.4 |
3099 |
30.39 |
235.8 |
0.1243 |
90.9 |
+ LR-101 (2)
|
8.9
|
1952
|
11.1
|
2442
|
235
|
0.0046
|
2.6
|
Bell 8048
|
Bell 8081
|
Bell 8247 (similar 8096)
|
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 |
D Ascent |
Bell 8247
|
|
|
71.7 |
2873 |
6.112 |
245 |
0.0249 |
17.6 |
Able 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 |
|
AJ-10-101A
|
|
|
33.4 |
2648 |
1.575 |
125 |
0.0126 |
4.17 |
|