Propulsion Atlas V |
Atlas V 400, 500 |
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 | ||||||
SRB |
AJ-60A |
max | 1,508.0 | 2447 | max | 1,688.3 | 2739 | 42.63 | 93.8 | max | 0.6164 | 116.8 | |
ave | 1,112.1 | ave | 1,245.2 | ave | 0.4545 | ||||||||
CCB |
RD-180 |
100% |
3,826.2 | 3059 | 4,152.4 | 3318 | 284.089 | 227 | 1.2534 | 942.6 | |||
D-5 (SEC) |
RL-10A-4-2 |
97.9 | 4378 | 20.830 | 932 | 0.0224 | 91.2 | ||||||
RL-10A-4-2N |
99.2 | 4423 | 20.830 | 928 | 0.0224 | 92.1 | |||||||
D-5 (SEC) |
RL-10C-1 |
101.9 | 4410 | 20.830 | 902 | 0.0231 | 91.8 | ||||||
D-5 (DEC) |
RL-10C-1 |
203.7 | 4410 | 20.83 | 451 | 0.0462 | 91.8 |
Atlas V HLV |
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 | |||
CCB (add.) |
RD-180 |
100% |
3,826.2 | 3059 | 4,152.4 | 3318 | 284.089 | 227 | 1.2534 | 942.6 |
CCB |
RD-180 |
100% |
3,826.2 | 3059 | 4,152.4 | 3318 | 284.089 | 227 | 1.2534 | 942.6 |
D-5 (SEC) |
RL-10A-4-2 |
97.9 | 4378 | 20.830 | 932 | 0.0224 | 91.2 |