|
|
|
| Propulsion H3 NGLV |
|
|
|
|
H-X (2011) |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn.time |
Flow rate |
Total Imp |
|
kN |
Ns/kg |
kN |
Ns/kg |
t |
s |
t/s |
MN*s |
||
| Booster (1) |
LE-X (2) |
||||||||
| 1 |
LE-X (2) |
||||||||
|
2 or |
LE-5B+ |
|
|
137.5 |
4393 |
|
|
0.0313 |
|
|
MB-60 |
|
|
266.9 |
4580 |
|
|
0.0583 |
|
|
|
3 or |
MB-35 |
|
|
155.7 |
4590 |
|
|
0.0339 |
|
|
LE-8 |
97.8 | 3383 | 0.0289 |
|
H-3 (2016) |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn.time |
Flow rate |
Total Imp |
||||
|
kN |
Ns/kg |
kN |
Ns/kg |
t |
s |
t/s |
MN*s |
||||||
| Booster (1) |
SRB-3 |
max | 2,233.5 | 2589 | max | 2,402.6 | 2785 | 66.80 | 105 | max | 0.6362 | 186.0 | |
| av | 1,647.0 | av | 1,771.7 | av | 0.8627 | ||||||||
| Booster (1) |
LE-9 (2) |
100% | 2,443.7 | 3462 | 2,942.0 | 4168 | 227.20 | 322 | 0.7059 | 946.9 | |||
|
1 or |
LE-9 (2) |
2,443.7 | 3462 | 2,940.0 | 4168 | 227.2 | 322 | 0.7059 | 946.9 | ||||
|
LE-9 (3) |
3,665.6 | 4,413.0 | 203 | 1.0588 | |||||||||
|
2 |
LE-5B-3 |
|
|
137.5 |
4393 |
25.0 |
800 |
0.0313 |
109.8 |
||||
|
|
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