|
Propulsion Tsiklon
|
Tsiklon-2
(R-36-O)
|
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
|
RD-251M
|
2,364.7 |
2644 |
2,643.7 |
2956 |
115.58 |
112.5 |
0.8945 |
340.3 |
|
RD-855 (4)
|
285.4
|
2443
|
334.6 |
2865 |
128 |
0.1148 |
|
2
|
RD-252
|
|
|
940.5 |
3115 |
45.61 |
140 |
0.3020 |
140.8 |
|
RD-856 (4)
|
|
|
53.95 |
2752 |
170 |
0.0196 |
|
FOBS
|
RD-854
|
|
|
75.50 |
3062 |
|
|
0.0247
|
|
|
Tsiklon
-2M
|
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
|
RD-261 (3)
|
2,364.7 |
2644 |
2,643.7 |
2956 |
129.62 |
120 |
0.8945 |
360.1 |
|
RD-855 (4)
|
285.4
|
2443
|
334.6 |
2865 |
128 |
0.1168 |
|
2
|
RD-262
|
|
|
940.5 |
3115 |
49.08 |
151.5 |
0.3020 |
151.7 |
|
RD-856 (4)
|
|
|
53.95 |
2752 |
170 |
0.0196 |
|
Tsiklon -3
|
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
|
RD-261 (3)
|
2,364.7 |
2644 |
2,643.7 |
2956 |
129.62 |
120 |
0.8945 |
360.1 |
| RD-855
(4) |
285.4
|
2443
|
334.6 |
2865 |
128 |
0.1168 |
|
2
|
RD-262
|
|
|
940.5 |
3115 |
49.08 |
151.5 |
0.3020 |
151.7 |
|
RD-856 (4)
|
|
|
53.95 |
2752 |
170 |
0.0196 |
|
PBV
|
RD-861
|
|
|
78.71 |
3109 |
3.19 |
126 |
0.0253 |
9.9 |
|
Tsiklon -2K
|
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
|
RD-261M (3)
|
2,364.7 |
2644 |
2,643.7 |
2956 |
129.62 |
120 |
0.8945 |
360.1 |
|
RD-855 (4)
|
285.4
|
2443
|
334.6 |
2865 |
128 |
0.1168 |
|
2
|
RD-262M
|
|
|
940.5 |
3115 |
49.08 |
151.5 |
0.3020 |
151.7 |
|
RD-856 (4)
|
|
|
53.95 |
2752 |
170 |
0.0196 |
|
ADU-600
|
S7.21 (4) ?
|
|
|
2.44 |
2952 |
0.600 |
720 |
0.008 |
1.8 |
|
