|
Propulsion Nositel (N) -1
|
NK-15
|
NK-15V
|
NK-21
|
NK-9V
|
RD-58
|
N-1 /1L...2L
(not launched)
|
Stage
|
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
|
|
Block A |
NK-15
(30)
|
41,358.3 |
2785 |
46,309.6 |
3118 |
1,743.4 |
25 |
14.8500 |
1,157.7 |
|
NK-15
(24)
|
33,086.6 |
37,047.7 |
113 |
11.8800 |
4,186.4 |
|
NK-15
(6)
|
8,271.6 |
9,291.9 |
10 |
2.9700 |
92.6 |
|
Block B |
NK-15V (8)
|
|
|
13,182.0 |
3187 |
504.6 |
110 |
4.1360 |
1,450.0 |
|
NK-15V (4)
|
6,561.0 |
24 |
2.0680 |
158.2 |
|
Block W |
NK-9V
(4)
|
|
|
1,804.4 |
3383 |
175.0 |
328 |
0.5333 |
592.1 |
|
Block G
|
NK-9V
|
|
|
451.1 |
33383 |
56.0 |
420 |
0.1333 |
189.5 |
|
Block D
|
NK-9V
|
|
|
451.1 |
3383 |
14.6 |
109.5 |
0.1333 |
49.4 |
N-1 /3...5L
|
Stage
|
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
|
|
Block A |
NK-15
(30)
|
41,358.3 |
2785 |
46,309.6 |
3118 |
1,743.4 |
25 |
14.8500 |
1,157.7 |
|
NK-15
(24)
|
33,086.6 |
37,047.7 |
113 |
11.8800 |
4,186.4 |
|
NK-15
(6)
|
8,271.6 |
9,291.9 |
10 |
2.9700 |
92.6 |
|
Block B |
NK-15V (8)
|
|
|
13,182.0 |
3187 |
504.6 |
110 |
4.1360 |
1,450.0 |
|
NK-15V (4)
|
6,561.0 |
24 |
2.0680 |
158.2 |
|
Block W |
NK-19
(4)
|
|
|
1,804,4 |
3383 |
175.0 |
328 |
0,5333 |
592.1 |
|
Block G
|
NK-21
|
|
|
392.3 |
3334 |
56.0 |
480 |
0.1177 |
186.7 |
|
Block D
|
RD-58
|
|
|
82.6 |
3393 |
14.6 |
600 |
0.0243 |
49.6 |
N-1 /6L ... 7L
|
Stage
|
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
|
|
Block A |
NK-15 (30)
|
41,358.3 |
2785 |
46,309.6 |
3118 |
1,743.4 |
25 |
14.8500 |
1,157.7 |
|
NK-15 (24)
|
33,086.6 |
37,047.7 |
113 |
11.8800 |
4,186.4 |
|
NK-15
(6)
|
8,271.6 |
9,291.9 |
10 |
2.9700 |
92.6 |
|
Block B |
NK-15V (8)
|
|
|
13,182.0 |
3187 |
504.6 |
110 |
4.1360 |
1,450.0 |
|
NK-15V (4)
|
6,561.0 |
24 |
2.0680 |
158.2 |
|
Block W |
NK-39
(4)
|
|
|
1,627.9 |
3452 |
175.0 |
371 |
0.4716 |
604.1 |
|
Block G
|
NK-31
|
|
|
402.1 |
3462 |
56.0 |
482 |
0.1162 |
193.9 |
|
Block D
|
RD-58
|
|
|
82.6 |
3393 |
14.6 |
600 |
0.0243 |
49.6 |
N-1F (not launched)
|
Stage
|
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
|
|
Block A* |
NK-33 (30)
|
100%) |
45,305.7 |
2915 |
50,458.1 |
3246 |
1,750.3 |
25 |
15.5448 |
1,261.5 |
|
80% |
36,244.5 |
40,366.5 |
107 |
12.4397 |
4,312.3 |
|
NK33 (8)
|
80% |
12,081.5 |
13,455.5 |
10 |
7.7724 |
107.6 |
|
Block B* |
NK-43 (8)
|
100% |
|
|
14,058.8 |
3393 |
505.5 |
110 |
4.1434 |
1,546.5 |
|
50% |
|
|
7,029.4 |
24 |
2.0717 |
168.7 |
|
Block W |
NK-39 (4)
|
|
|
1,627.9 |
3452 |
175.0 |
371 |
0.4716 |
604.1 |
|
Block G
|
NK-31
|
|
|
402.1 |
3462 |
56.0 |
482 |
0.1162 |
193.9 |
|
Block D
|
RD-58
|
|
|
82.6 |
3393 |
14.6 |
600 |
0.0243 |
49.6 |
*
Engines are throttleable
N-1M (project)
|
Block W |
RD-57
(4)
|
|
|
1,569.2 |
4477 |
|
|
0.3505 |
|
|
Block G
|
RD-57
|
|
|
392.3 |
4477 |
|
|
0.0876 |
|
|
Block D
|
RD-58
|
|
|
82.6 |
3393 |
14.60 |
600 |
0.0243 |
49.6 |
|
