The first Soviet S-25 SAM-system V-300
(Berkut)
-- Some images to this unique
liquid fueled missiles --
Norbert Brügge, Germany
The
V-300 (Berkut) was the first surface-to-air missile deployed by the Soviet
Union. The V-300 is a single-stage liquid fueled missile. The development
began in 1950, first guided launch was in 1953, and by 1956, more as thoused
of launchers were deployed in defence around Moscow. The system was upgraded
with improved missiles and ground systems into the 1960's.
At the end of 1950 Isayev's OKB-2 began development of the 9 tonne thrust
engine for the missile. This was based on the four-chamber R101B-3600 in development
for the R-101B. The resulting engine for the first V-300/La205 missile,
the S09.29.0-0, differed from the R101B-3600 only in a beefed-up structure
and propellant feed lines. The engine was pressure-fed using a ram air compression
system.
Further factory trials of the engine planned for the V-300/La205 missile showed
that the loss of the hermetic seal in the chamber head resulted in thrust
oscillations. The fix was a version with a sealed chamber head, designated
S09.29.0-0B. In 1952 this modification was mounted in a V-300/La205 airframe.
In 1953, after the death of Stalin, the Berkut system was redesignated
S-25.
Missile
|
Engine (OKB
Isayev)
|
Propellant
|
Remark
|
La205
|
S09.29.0-0B
(4)
|
TG-02/AK-20
|
|
La206
|
S2.145
|
La205 with
single engine S2.145; canceled
|
La207
|
S09.29.0-0V
(4)
|
Isayev has
planned single engine S2.145
|
La207A
|
S2.260
|
TG-02/AK-20F
|
|
La208
|
S09.29.0-0B
(4)
|
TG-02/AK-20
|
La207A with
other engine; canceled
|
La215
|
S2.260
|
TG-02/AK-20F
|
La207A with
nuclear WH
|
La217A
|
S2.751B
|
TG-02/AK-20K
|
|
La217M
|
S5.1
|
TG-02/AK-20K
|
|
La217MA
|
S5.41
|
TG-02/AK-27I
|
|
La217MAM
|
S5.44
|
core 5Ya25
|
La218
|
S5.1 |
La217M with nuclear
WH |
La219
|
S5.44 (variant)
|
La217MAM with
core 5Ya24
|
La205
La207
|
La205
|
S09.29.0
S2.145
(planned)
|
La217A
|
|
|
La217MA
La217MAM
La219
|
|
S5.44 engine
|
RM-75
Target
|
On the basis of V-300 anti-aircraft rocket La217MA which expired their
service life, there were designed, tested and put into the serial production
the following types of the RM-75 rocket-targets: KUNITSA
(1965-1970), SOBOL (1970-1975), BELKA (1975-1988), ZVEZDA
(1988-1993) and STRIZH (1994 to the present time).
The rocket-target RM-75 consist of two modifications: RM-75MV for
low altitudes and RM-75V for high altitude.
|
|