|
Some identified rocket-engines
from Isayev's Design Bureau (now KB Khimmash)
Norbert Brügge, Germany
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
aircraft |
|
S3.40 |
|
1 |
|
TG-02 |
AK-20 |
|
|
|
|
|
Project R-12 |
|
S3.41 |
|
4 |
|
TG-02 |
AK-20 |
|
|
|
|
|
S3.42A |
|
1 |
1 |
TG-02 |
AK-20 |
154.1 |
|
|
|
V-300 |
Project
La217 |
|
S3.42T-3 |
|
1 |
1 |
TM-185 |
AK-27 |
|
|
|
|
"Scud" |
R-11MU/R-17-1 |
|
S3.46
|
|
|
|
|
|
|
|
|
|
|
Project R-16 |
|
S3.50
|
|
|
|
|
|
|
|
|
|
|
S3.52
|
|
8 |
|
|
|
|
|
|
|
|
Project R-15 SLBM |
|
S3.54
|
|
4 |
|
|
|
|
|
|
|
|
S3.55
|
|
|
|
|
|
|
|
|
|
|
Project R-16 |
|
S3.56
|
|
|
|
|
|
|
|
|
|
|
S3.61
|
|
|
|
|
|
|
|
|
|
|
Air defense systems
(V-300 "Berkut" etc.) |
| S09.29 |
Sevruk type ? |
4 |
1 |
TG-02 |
AK-20F |
78.4 |
? |
88.2 |
? |
V-300 |
La205,
La207 |
| S2.145 |
Sevruk type |
1 |
1 |
TG-02 |
AK-20F |
83.4 |
? |
88.2 |
? |
|
|
S2.244
|
Sevruk type |
1 |
1 |
TG-02 |
AK-20F |
|
|
|
|
|
|
S2.260
|
Sevruk type |
1 |
1 |
TG-02 |
AK-20F |
|
|
|
|
La207A |
|
S2.751V
|
|
1 |
1 |
TG-02 |
AK-20K |
157.9 |
|
|
|
La217A |
|
S5.1
|
S5.1A |
1 |
1 |
TG-02 |
AK-20I |
168.5 |
|
|
|
La217M, La218
|
| S5.44 |
5D25 |
1 |
1 |
TG-02 |
AK-27I |
181.4 |
2461 |
? |
? |
La217MA |
| S2.168
? |
Sevruk type |
1 |
2 |
TG-02 |
AK-20F |
|
|
|
|
|
? |
|
S2.168B |
Sevruk type |
1 |
2 |
TG-02 |
AK-20F |
11.5 |
2118 |
12.3 |
2265 |
ShB-32 |
|
| S2.711 |
|
1 |
2 |
TG-02 |
AK-20F |
26.0 |
2197 |
29.4 |
2478 |
V-750
|
S-75
(Dvina)
|
| S2.711V |
|
1 |
2 |
TG-02 |
AK-20F |
30.4 |
2355 |
33.85 |
|
V-750V |
| S2.711V1 |
|
1 |
2 |
TG-02 |
AK-20F |
|
|
|
|
| S2.711V2 |
|
1 |
2 |
TG-02 |
AK-20F |
|
|
|
|
|
S2.711V
deriv. |
|
2x1 |
1 |
TG-02 |
AK-20K |
|
|
|
|
India's
Prithvi SRBM |
| S2.720 |
|
1 |
2 |
TG-02 |
AK-20K |
34.3 |
2300 |
? |
? |
V-750VM |
Dvina-M |
| S2.720A |
|
1 |
2 |
TG-02 |
AK-20K |
|
|
|
|
V-750VN |
Desna |
|
S2.720 deriv.
|
|
1 |
1 |
TG-02 |
AK-20K |
|
|
|
|
Iraqi
Al-Samoud |
|
S2.720A2 |
|
1 |
2 |
TG-02 |
AK-20K |
|
|
|
|
V-755
V-759
|
S-75M
Volchov/5Ya23 |
|
|
1 |
2 |
TG-02 |
AK-20K |
|
|
|
|
|
TRM-3500 |
|
1 |
- |
JP-4 |
AK-20K |
35.0 |
2215 |
|
|
Developed by EDEPRO, Serbia |
|
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 |
|
S5.33A1
|
|
2 |
- |
TG-02 |
AK-27I |
56.7 |
2795 |
- |
- |
ASM |
KSR-3 |
|
S5.33A2
|
|
2 |
- |
TG-02 |
AK-27I |
69.6 |
? |
- |
- |
ASM |
KSR-5 |
| R-201-300 |
|
2 |
- |
TG-02 |
AK-27I |
83.0 |
? |
- |
- |
ASM |
KH-22 |
|
Various missiles |
|
S2.1100
|
|
4 |
1 |
TG-02 |
AK-27I |
671.2 |
2285 |
749.0 |
2550 |
Burya booster |
|
S2.1150
|
|
4 |
1 |
TG-02 |
AK-27I |
672.9 |
2314 |
750.0 |
2579 |
Burya booster |
|
S2.253
|
Sevruk
type ? |
1 |
1 |
T-1 |
AK-20F |
81.4 |
2148 |
94.8 |
2501 |
R-11 (Scud-A) |
|
S5.2
|
9D21 |
1 |
1 |
TM-185 |
AK-27I |
132.1 |
2285 |
146.3 |
2530 |
R-17 (Scud-B)
|
|
S2.713
|
5D50 |
1+4V |
1 |
TG-02 |
AK-27I |
252.1 |
2275 |
274.0 |
2466 |
R-13 SLBM
|
|
S5.3M
|
|
4 |
1 |
TG-02 |
AK-27I |
398.8 |
2367 |
423.3 |
2511 |
R-21 SLMB |
|
?
|
4D10
|
1+2V |
1 |
UDMH |
AK-27P |
216.5 |
2579 |
238.7 |
2844 |
R-27 SLBM |
|
?
|
4D20 |
1+2V |
1 |
UDMH |
N2O4 |
233.9 |
2638 |
257.4 |
2903 |
R-27U SLBM |
|
?
|
4D18 |
1+2V |
1 |
UDMH |
N2O4 |
|
|
|
|
R-27K SLBM |
|
?
|
4D19 |
1+8V |
2 |
UDMH |
N2O4 |
|
|
|
|
|
?
|
3D37 |
1 |
1 |
UDMH |
N2O4 |
|
|
|
|
R-29 "Vysota" SLBM |
|
?
|
3D38 |
1 |
2 |
UDMH |
N2O4 |
|
|
|
|
|
?
|
4D75 |
1+4V |
1 |
UDMH |
N2O4 |
|
2802 |
|
3124 |
R-29R "Volna" SLBM |
|
?
|
4D76 |
1 + V |
2 |
UDMH |
N2O4 |
|
|
|
|
|
?
|
3D41
|
1 + V |
2 |
UDMH |
N2O4 |
|
|
|
|
R-29RM SLBM |
|
Izotov & Mevius design
* |
| 15D13 |
5D22 |
1 |
2 |
UDMH |
N2O4 |
|
|
|
|
UR-100 ICBM |
| 15D14 |
|
4 x
1V |
|
|
|
|
| 15D14 |
|
1 |
- |
|
|
|
|
Almaz space station |
|
5D12
(S2.726 ?) |
designed by
Mevius
|
1 |
1 |
TG-02 |
AK-27P |
98.0 |
|
|
|
V-860 |
S-200
Angara/Vega/Dubna |
|
5D67 |
1 |
1 |
TG-02 |
AK-27P |
103.0 |
|
|
|
V-880 |
|
5D67
|
1 |
1 |
TG-02 |
AK-27P |
|
|
|
|
Scramjet |
|
5D16
|
1 |
2 |
? |
? |
156.9 |
|
|
|
A-350 "Galosh" |
|
5D22
|
1 |
2 |
UDMH |
N2O4 |
131.4 |
|
|
|
A-350 "Galosh" |
|
5D18
|
4 x 1V |
31.4 |
|
|
|
|
5D21M
|
1 |
Booster |
|
|
|
|
|
|
Spaceplan "Spiral" |
|
Kosberg design
(former Isayev design)* |
| RD-0200 |
S2.1200 |
2 |
2 |
TG-02 |
AK-27I |
58.8 |
2256 |
|
|
V-400 |
"Dalh" |
|
RD-0200A ?
|
S2.1200A ?
|
2 |
2 |
|
|
|
|
|
|
|
|
| RD-0201 |
S2.1201 |
4 |
3 |
TG-02 |
AK-27P |
|
|
|
|
V-1100 |
Project |
|
Dushkin design |
| RU-013 |
Sevruk
type ? |
1 |
Booster |
TG-02 |
AK-20 |
31.0 |
|
|
|
|
MIG
aircraft |
|
S2.711
|
S2.711
(Iran)
|
S2.711V
|
S2.711V1
|
S2.711V1
|
S2.711V2
|
|
S2.711
(Prithvi)
|
S2.711V (Iran)
|
|
S2.720
|
S2.720
|
S2.720
|
S2.720
|
S2.720
|
S2.720
|
S2.720 |
S2.720 |
S2.720 |
|
S2.720A
|
|
|
|
S2.720 (Iran) |
S2.720 (Iran) |
S2.720 (Iran)
|
S2.720 (Al-Samoud)
|
|
|
