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| Propulsion L & Mu |
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L-4S |
Motor |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
|
kN (av.) |
N*s/kg |
kN (av.) |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
| Booster |
SB-310 |
95.0 | 2157 | 107.9 | 2452 | 0.312 | 7.1 | 0.0440 | 0.8 |
| 1 |
L-10 |
295.1 | 2108 | 362.9 | 2403 | 3.887 | 27.8 | 0.1400 | 9.3 |
|
2 |
L-20 |
115.7 | 2382 | 1.845 | 38 | 0.0486 | 4.4 | ||
|
3 |
L-30 |
64.7 | 2445 | 0.548 | 20.7 | 0.0265 | 1.3 | ||
| 4 |
L-40 |
7.8 | 2491 | 0.088 | 27.5 | 0.0032 | 0.2 |
|
M-4S |
Motor |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
|
kN (av.) |
N*s/kg |
kN (av.) |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
|
Booster |
SB-310 |
94.6 | 2148 | 107.9 | 2452 | 0.337 | 7.7 | 0.0440 | 0.8 |
|
1 |
M-10 |
730.1 | 2148 | 833.6 | 2452 | 20.522 | 60.4 | 0.3400 | 50.3 |
|
2 |
M-20 |
284.4 | 2559 | 7.146 | 64.3 | 0.1111 | 18.3 | ||
|
3 |
M-30 |
129.4 | 2599 | 1.986 | 39.9 | 0.0498 | 5.2 | ||
| 4 |
M-40 |
26.5 | 2648 | 0.369 | 37 | 0.0100 | 1.0 |
|
M-3C |
Motor |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
|
kN (av.) |
N*s/kg |
kN (av.) |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
|
Booster |
SB-310 |
94.6 | 2148 | 107.9 | 2452 | 0.337 | 7.7 | 0.0440 | 0.8 |
|
1 |
M-11 |
762.5 | 2185 | 865.9 | 2481 | 20.453 | 58.6 | 0.3490 | 50.7 |
|
2 |
M-21 |
278.5 | 2677 | 7.174 | 68.7 | 0.1040 | 19.1 | ||
|
3 |
M-3A |
56.9 | 2775 | 1.075 | 52.5 | 0.0205 | 3.0 |
|
M-3H |
Motor |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
|
kN (av.) |
N*s/kg |
kN (av.) |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
|
Booster |
SB-310 |
94.6 | 2148 | 107.9 | 2452 | 0.342 | 7.8 | 0.0440 | 0.8 |
|
1 |
M-12 |
969.1 | 2344 | 1,078.7 | 2608 | 27.098 | 65.5 | 0.4135 | 70.6 |
|
2 |
M-22 |
324.6 | 2716 | 7.195 | 60.2 | 0.1195 | 19.6 | ||
|
3 |
M-3A |
56.9 | 2785 | 1.084 | 53.1 | 0.0204 | 3.0 |
|
M-3SI |
Motor |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
|
kN (av.) |
N*s/kg |
kN (av.) |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
|
Booster |
SB-310 |
94.6 |
2148 |
107.9 |
2452 |
0.343 |
7.8 |
0.0440 |
0.8 |
|
1 |
M-13 TVC |
1,134.3 |
2344 |
1,262.6 |
2608 |
27.064 |
56.0 |
0.4840 |
70.6 |
|
2 |
M-22 TVC |
324.6 | 2716 | 7.201 | 60.2 | 0.1195 | 19.6 | ||
|
3 |
M-3A |
56.9 | 2785 | 1.084 | 53.1 | 0.0204 | 3.0 |
|
M-3SII |
Motor |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
|
kN (av.) |
N*s/kg |
kN (av.) |
N*s/kg |
tons |
s |
t/s |
MN*s |
||
|
Booster |
SB-735 TVC |
303.6 | 2344 | 337.8 | 2608 | 4.012 | 31.0 | 0.1295 | 10.5 |
|
1 |
M-13 TVC |
1,134.3 | 2344 | 1,262.6 | 2608 | 27.098 | 56.0 | 0.4840 | 70.7 |
|
2 |
M-23 TVC |
524.6 | 2765 | 10.317 | 54.5 | 0.1897 | 28.5 | ||
|
3 |
M-3B |
132.0 | 2874 | 3.298 | 71.9 | 0.0459 | 9.5 |
