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Propulsion Ares I (CLV) & Ares V (CaLV)
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Ares I (2008)
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Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
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| kN | N*s/kg | kN | N*s/kg | tons | sec | t/s | MN*s | |||||
| 1 | RSRM (5-segments) | max | 16,201.5 | 2373 | max | 17,882.0 | 2619 | 647.653 | 131.9 | max | 6.8269 | 1,696.42 |
| ave | 11,651.1 | ave | 12,859.6 | ave | 4.9095 | |||||||
| 2 | J-2X (1) | 1,307.5 | 4393 | 137.08 | 460.6 | 0.2976 | 602.2 | |||||
Ares V (2008)
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Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
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| kN | N*s/kg | kN (max) | N*s/kg | tons | sec | t/s | MN*s | |||||
| Booster | RSRM (5.5 segments) | max | 16,651.0 | 2373 | max | 18,371.5 | 2618 | 711.157 | 133 | max | 7.0164 | 1,862.07 |
| ave | 12,689.6 | ave | 14,000.5 | ave | 5.3470 | |||||||
| 1 | RS-68B (6) | 18,976.2 | 3657 | 21,271.8 | 4099 | 1.587.37 | 305.9 | 5.1894 | 6,506.6 | |||
| 2 | J-2X (1) | 1,307.5 | 4393 | 251.84 | 846.1 | 0.2976 | 1,106.4 | |||||
Note: Data of RSRM are calculated
