|
Some identified rocket-engines
from Isayev's Design Bureau (now KB Khimmash)
Norbert Brügge, Germany
Update: 17.05.2013
Throughout
its history the Isayev Design Bureau OKB-2 has created since 1953 more than
120 liquid-fuel engines and engine assemblies for missiles and spacecrafts.
Approximately 40 of these engine designs proceeded into serial production.
Here are some data and pictures, which I found up to now.
Some of them are similar to Isayev's engines, but of other designers (e.g.
OKB Sevruk; in 1958 with Isayev's OKB-2 fusioned)*.
|
Engine designation
|
Chamb. |
Stage |
Propellant |
Thrust s.l
(kN) |
Isp s.l.
(Nskg) |
Thrust vac
(kN) |
Isp vac
(Nskg) |
Vehicle |
|
Fuel |
Oxidiser |
| OKB-3 Sevruk* |
| S3.20M |
|
1 |
booster |
TG-02 |
AK-20 |
31.4 |
|
|
|
|
MiG-19Su |
| S3.40 |
|
1 |
1th |
TG-02 |
AK-20 |
|
|
|
|
|
|
| S3.41 |
|
4 |
1th |
TG-02 |
AK-27 |
|
|
|
|
|
R-15 SLBM |
| S3.42A |
|
1 |
1th |
TG-02 |
AK-20 |
|
|
|
|
V-300 |
La217 |
| S3.42T-3 |
|
1 |
1th |
TM-185 |
AK-27 |
|
|
|
|
"Scud" |
R-11MU/R-17-1 |
| Air defense
systems (V-300 "Berkut" etc.) |
| S09.29 |
Sevruk type ? |
4 |
1th |
TG-02 |
AK-20F |
78.4 |
? |
88.2 |
? |
V-300 |
La205, La207 |
| S2.145 |
Sevruk type |
1 |
1th |
TG-02 |
AK-20F |
83.4 |
? |
88.2 |
? |
|
|
S2.244
|
Sevruk type |
1 |
1th |
TG-02 |
AK-20F |
|
|
|
|
|
|
S2.260
|
Sevruk type |
1 |
1th |
TG-02 |
AK-20F |
|
|
|
|
La207A |
|
S2.751V
|
|
1 |
1th |
TG-02 |
AK-20K |
157.9 |
|
|
|
La217A |
|
S5.1
|
|
1 |
1th |
TG-02 |
AK-20I |
168.5 |
|
|
|
La217M, La218
|
|
S5.41
|
5D25 |
1 |
1th |
TG-02 |
AK-27I |
|
|
|
|
La217MA |
| S5.44 |
|
1 |
1th |
TG-02 |
AK-27I |
181.4 |
2461 |
? |
? |
La217MA |
| S2.168 ? |
Sevruk type |
1 |
2th |
TG-02 |
AK-20F |
|
|
|
|
|
? |
| S2.168B |
Sevruk type |
1 |
2th |
TG-02 |
AK-20F |
11.5 |
2118 |
12.3 |
2265 |
ShB-32 |
|
| S2.711 |
|
1 |
2th |
TG-02 |
AK-20F |
26.0 |
2197 |
29.4 |
2478 |
V-750
|
S-75
(Dvina)
|
| S2.711V |
|
1 |
2th |
TG-02 |
AK-20F |
30.4 |
? |
33.85 |
? |
V-750V |
| S2.711V1 |
|
1 |
2th |
TG-02 |
AK-20F |
|
|
|
|
| S2.711V2 |
|
1 |
2th |
TG-02 |
AK-20F |
|
|
|
|
|
S2.711V
deriv. |
|
2x1 |
1th |
TG-02 |
AK-20K |
|
|
|
|
India's Prithvi SRBM |
| S2.720 |
|
1 |
2th |
TG-02 |
AK-20K |
34.3 |
2285 |
? |
? |
V-750VM |
Dvina-M |
| S2.720A |
|
1 |
2th |
TG-02 |
AK-20K |
|
|
|
|
V-750VN |
Desna |
| S2.720A1 |
|
1 |
2th |
TG-02 |
AK-20K |
|
|
|
|
V-755
V-759
|
S-75M
Volchov/5Ya23 |
| S2.720A2 |
|
1 |
2th |
TG-02 |
AK-20K |
|
|
|
|
|
TRM-3500 |
|
1 |
- |
JP-4 |
AK-20K |
35.0 |
2215 |
|
|
Developed by EDEPRO, Serbia |
|
|
5D12 |
1 |
1th |
TG-02 |
AK-20K |
|
|
|
|
V-860
V-880 |
S-200
Angara/Vega/Dubna |
| S2.726
? |
5D67 |
1 |
1th |
TG-02 |
AK-20K |
101.0 |
? |
|
|
|
S2.727
|
|
1 |
2th |
|
|
|
|
|
|
Krug |
|
S5.15
|
|
1 |
2th |
|
|
|
|
|
|
Krug-M |
| Anti-ship missiles |
|
S2.721
|
|
1 |
- |
TG-02 |
AK-20F |
12.2 |
? |
- |
- |
ASM |
KSR |
|
S2.722
|
|
1 |
- |
TG-02 |
AK-20K |
11.9 |
? |
- |
- |
ASM |
P-15 (Hy-2) |
| S2.722V |
|
1 |
- |
TG-02 |
AK-20K |
|
|
- |
- |
|
S5.6
|
|
1 |
- |
TG-02 |
AK-20K |
11.8 |
? |
- |
- |
ASM |
KSR-2 |
|
S5.33
|
|
2 |
- |
TG-02 |
AK-27I |
56.7 |
2795 |
- |
- |
ASM |
KSR-5 |
|
S5.33A
|
|
2 |
- |
TG-02 |
AK-27I |
69.6 |
? |
- |
- |
ASM |
KSR-5H
etc. |
| Various missiles |
|
S2.1100
|
|
4 |
1th |
TG-02 |
AK-27I |
671.2 |
2285 |
749.0 |
2550 |
Burya booster |
|
S2.1150
|
|
4 |
1st |
TG-02 |
AK-27I |
672.9 |
2314 |
750.0 |
2579 |
Burya booster |
|
S2.253
|
Sevruk type ? |
1 |
1th |
T-1 |
AK-20F |
81.4 |
2148 |
94.8 |
2501 |
R-11 (Scud-A) |
|
S5.2
|
9D21 |
1 |
1th |
TM-185 |
AK-27I |
132.1 |
2285 |
146.3 |
2530 |
R-17 (Scud-B)
|
|
S2.713
|
5D50 |
1+4V |
1th |
TG-02 |
AK-27I |
252.1 |
2275 |
274.0 |
2466 |
R-13 SLBM
|
|
S5.3M
|
|
4 |
1th |
TG-02 |
AK-27I |
398.8 |
2367 |
423.3 |
2511 |
R-21 SLMB |
| ? |
4D10
|
1+2V |
1th |
UDMH |
AK-27P |
216.5 |
2579 |
238.7 |
2844 |
R-27 SLBM |
| |
4D10 |
1+2V |
1th |
UDMH |
N2O4 |
233.9 |
2638 |
257.4 |
2903 |
R-27U SLBM |
| ? |
4D18 |
1+2V |
1th |
UDMH |
N2O4 |
|
|
|
|
R-27K
SLBM |
| ? |
4D19 |
1+8V |
2th |
UDMH |
N2O4 |
|
|
|
|
| ? |
4D75 |
1+4V |
1th |
UDMH |
N2O4 |
|
|
|
|
R-29R
SLBM |
| ? |
4D76 |
1 |
2th |
UDMH |
N2O4 |
|
|
|
|
| Izotov design* |
| 5D22 |
15D13 |
1 |
2th |
UDMH |
N2O4 |
|
|
|
|
UR-100
ICBM |
| RK-3 |
15D14 |
4 x 1V |
|
|
|
|
| RK-2 |
|
1 |
- |
|
|
|
|
|
|
Almaz space station |
| 5D67 |
Meviusa
|
1 |
1th |
TG-02 |
AK-27P |
103.0 |
? |
|
|
V-880 |
S-200 |
| 5D21M |
|
1 |
- |
|
|
|
|
|
|
Spaceplan "Spiral" |
| Kosberg
design
(former Isayev design)* |
| RD-0200 |
S2.2100 |
2 |
2th |
TG-02 |
AK-27I |
|
|
|
|
V-400 |
"Dalh" |
| RD-0201 |
S2.2101 |
4 |
3th |
TG-02 |
AK-27P |
58.8 |
2256 |
|
|
V-1100 |
Project |
| Dushkin design |
| RU-013 |
Sevruk type ? |
1 |
Booster |
TG-02 |
AK-20 |
31.0 |
|
|
|
|
MIG-19 |
Main source: Forum Novosti Kosmonavtiki
(Sergey Zdorikov, Odessa, Ukraine)
|
S2.711
|
S2.711V
|
S2.711V (Iran)
|
S2.711V1
|
S2.711V1
|
S2.711V2
|
S2.711_Prithvi
|
S2.720A
|
S2.720
|
|
S2.720
|
S2.720
|
S2.720
|
S2.720
|
S2.720
|
S2.720 |
S2.720 (Iran) |
S2.720 (Iran) |
S2.720 (Iran)
|
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