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| Propulsion KSLV-2 (Nuri) |
|
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|
Nuri |
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 |
||
| 1 |
URE-1 (4) |
2,626.0 | 2565 | 2,992.3 | 2923 | 131.33 | 128.3 | 1.0236 | 383.9 |
|
2 |
URE-2 |
791.5 | 3093 | 36.83 | 143.9 | 0.2559 | 113.9 | ||
|
3 |
URE-3 |
68.6 | 3188 | 10.81 | 502.1 | 0.0215 | 34.5 |
|
TLV |
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 |
||
| 1 |
URE-1 (1) |
652.7 | 2561 | 743.3 | 2918 | 36.7 | 143.5 | 0.2547 | 107.1 |
|
1* |
URE-1 (1) |
639.0 |
2567 |
728.1 |
2925 |
36.7 |
146.7 |
0.2489 |
107.4 |
| * really in test launch |
