Part III The BETAB Rocket-bomb
(Part I, Part II, Part IV)
One of the very interesting details which
modelers may apply
to their work are the external stores found on military aircraft. In a
way, these stores are the precise reason why many combat aircraft were
built, so they are by no means a mere curiosity nor diversion. In this
new series of articles, we will look at the various bombs, rockets,
missiles,
torpedoes, and countless other munitions carried by VVS aircraft of the
1930-50 period.
The 'Other RS'
During the 1930s, Soviet munitions designers were well
advanced in several areas of conceptual development. Amongst the most intriguing
of these was the concept of the rocket assisted bomb. Indeed, this work
was carried on in conjunction with the more commonly known RS rocket, to
which they were seen as an alternative and complimentary munition [and
with which they are routinely confused]. The development of the BETAB and
BRAB series rocket bombs was a highly complex matter, and we will only
touch upon the highlights of this story here.
In 1936, the Navy (VMF) asked one of the NII's many departments,
No.3, to undertake a study of superior armour-penetrating munitions for
use in anti-maritime aviation duties. These studies coincided with the
development of the RS rocket, and the department investigated versions
of the RS 132 missile for these purposes. There were many, many theoretical
plans in this regard (which by themselves could make for an entire book
on the subject), and by 1938 these had merged with an intention to develop
a 203 mm version of the RS. In the end, a 203 mm version of the RS was
seen to be impractical, however this size of munition was developed further
by the NII-3 in line with a new concept-- the rocket assisted bomb. Moreover,
the NII-3 had developed a new explosive type for this kind of weapon, this
named TM-4(b).
The concept of these munitions was straightforward, if
novel. The rocket motor was designed firstly to imbue the bomb, which was
to be released in the traditional manner (i.e. in level flight, or from
a shallow dive if required), with a more stable trajectory after release.
Secondly, the rocket motor would add to the kinetic energy of the bomb
upon impact, thus aiding its penetrative powers. In fact, both concepts
proved to be quite valid, but particularly so the latter. The thrust of
the rocket motor added enormously to the penetration of the munition, as
seen in the following NII-3 test results using the prototype 203 mm BETAB:
Bombs dropped from 2000 m against face-hardened concrete
| Bomb Type |
Penetration (mm) |
| FAB-100 |
400 |
| BETAB-203mm without rocket motor |
750 |
| BETAB-203mm with rocket motor fired |
1480 |
This outstanding penetration capability, married to improved
accuracy through a more stable trajectory, immediately caught the eye of
the VMF. The Navy recognized this kind of munition as an anti-shipping
weapon of exactly the type that they had requested in 1936. Thus, from
1938 onward, the VMF became inexorably intertwined in the development of
these bombs. Development was rapid, and testing was conducted at a vigorous
pace, reflecting the service's keen interest in this new munition. Indeed,
by 1939 the Navy had used its various connections to instigate production
of these weapons at Zavod 80 (NKB) under the designation BETAB-150DS.
The acronym 'BETAB' I do not currently understand fully, but the number
cipher was obtained from the weight of the munition, and suffix 'DS' stood
for s dopolnitel'nimi skorostyami, or 'with supplimental velocity'.
Navy BRABs
At the same time investigations were underway concerning
the future BETAB munition, the VMF was also interested in the development
of a new series of special purpose armour-piercing bombs. This new family
of bombs were intended specifically to penetrate the steel armour plate
of warships, and other related targets, and they acquired the designation
BRAB (broneboynie aviabombi, or 'armour-penetrating aviation bombs')
from the outset.
All manner of possible BRAB configurations were considered
and tested. In 1938, a 150 kg version with similar dimensions to the new
BETAB appeared, and this munition was seized upon immediately in the new
enthusiasm regarding rocket-bomb types. Thus, the NII-3 built and tested
several DS type 203 mm BRABs, these featuring the same rocket aft section
as the similar BETAB.
Bigger is Bureaucratic
As these programmes continued, Navy enthusiasm for rocket-bombs
reached astronomical proportions. BETAB and DS powered BRABs of increasingly
larger weight and calibre were continuously built and proposed. Further,
so engulfed did the VMF become in this development work, that the primary
Department of the NII in Leningrad, No.24, also was drawn fully into these
efforts by sheer proximity to the Navy's headquarters in that city. Indeed,
the NII-24 worked on munitions of 254 mm diameter-- resulting in the BRAB-500DS--
followed by even larger rocket-bombs of 305 mm size (such as the BETAB-750DS).
In fact, bigger bombs that these were actually built (the BRAB-800DS prototypes,
for example) by NII-24, but some of their proposals from 1940 read like
pure fiction; one BETAB was suggested at a staggering 3000 kg weight!!
However, such proposals were mere bureaucratic fancy.
Any engineer can attest that weight, thrust, and energy calculations do
not scale proportionally, and the larger the munitions became, the less
became their value as compared to more traditional AP bombs. Sanity managed
to prevail, and none of these colossal blunderbusses were ever constructed....
-------------------------------
Disregarding the many small series of experimental types--
some of which, admittedly, were in fact employed operationally during
the War, the following can be seen as the main series of BETAB and DS BRAB
munitions of the era.
BETAB-150DS 1940
Length: 2095 mm
Max. Diameter: 203 mm
Overall Weight: 163 kg
Weight of Explosive Filling: 17.10 kg |
 |
The original 203 mm calibre rocket bomb munition was this
weapon, the -150DS. The rear rocket motor housing was built separately,
and was standard for all of the munitions of 203 mm size. The fins were
welded to the housing, and were somewhat thick sheet metal, as was the
rocket casing itself. The forward portion of the bomb comprised the warhead,
this a 17 kg charge of TM-4(b) explosive surrounded by a thick, hardened
alloy steel sheath of ballistic shape. The model depicted here is typical
of manufacture from 1940, finished in the ubiquitous medium blue Soviet
industrial paint, and the standard aviation bomb lacquer No.67 was usually
applied to the munition before delivery.
The aft mounting strap was similar to that of a small
FAB, whilst the forward mounting strap featured an electrical receptor
socket at the tip. After release, a wire from the aircraft would detach
from this point and the rocket motor would fire after a small delay. Rocket
bombs were only carried externally, it being thought that internal storage
was vastly too dangerous (albeit, technically feasible on aircraft like
the Il-4 and Pe-2). The BETAB-150DS was utilized throughout the VMF, on
all fronts, and was seen well into 1943.
BETAB-150DS finished in lacquer No.67
BETAB-170DS 1942
Length: 2087 mm
Max. Diameter: 203 mm
Overall Weight: 170 kg
Weight of Explosive Filling: 15.3 kg |
 |
Manufacture of the BETAB-150DS model gave way gradually
to the -170DS during 1942. The new model was slightly shorter than the
-150DS, and carried less explosive filling in a warhead of thicker nickel-alloy
steel. The aft rocket housing was indentical, as previously mentioned.
The model depicted here is typical of manufacture from 1942-43, and is
finished in Industrial Metal Primer, which was very widely use for rocket
bomb production.
The BETAB-170DS remained in use with the VMF for many
years after the GPW, and was regarded as a very effective weapon. In fact,
so well regarded were BETAB-170s, that some Army regiments also made limited
use of them, presuambly having obtained them from nearby VMF units. Moreover,
authors Reznichenko and Pir'ev mention in their official VVS bomb history
that a variant of this munition remained in production and in the Soviet
aviation inventory, essentially unchanged, into the 1970s-- a pretty fair
claim to sucess, indeed.
BETAB-170DS finished in lacquer No.67
BRAB-200DS 1940
Length: 1710 mm
Max. Diameter: 203 mm
Overall Weight: 212 kg
Weight of Explosive Filling: 12.27 kg |
 |
Alongside the BETAB, the Navy also developed a rocket
version of the BRAB armour-piercing bomb. This munition was also of 203
mm calibre, and utilized the same rocket motor and housing as the BETABs
of the same size. The warhead, however, was indeed that of a BRAB bomb,
featuring a very sharply pointed AB-1(d) nickel-steel alloy casing. A small
protective cap, of light metal construction, was applied to the tip (presumably
to protect it and the armourers). The bomb is shown here in ALG-1
finish, as suggested by Reznichenko and Pir'ev.
Limited manufacture of the BRAB-200DS was undertaken prior
to the GPW at Zavod 78 (NKTM). Something like 3000 of these bombs
were completed by 1941, but production was terminated in favour of the
BETAB series, and the focus for the BRAB munition was thereafter on non-powered
bombs of larger calibre. Despite this fact, all of these weapons were used
operationally, until supplies were exhausted (perhaps during 1942?), and
they were noted for excellent armour penetration capabilities.
BRAB munition warhead, showing the protective cap
BRAB-500DS 1939
Length: 3220 mm
Max. Diameter: 254 mm
Overall Weight: 503.10 kg
Weight of Explosive Filling: 24.6 kg |
 |
The NII Department No.24 became heavily involved in the
development of larger and larger rocket-bombs. The basic design of the
rocket housing for these was unchanged, but the diameter in this case was
increaed to 254 mm, and consdierably lengthened (for additional propellant).
The warhead was similar to that of the smaller -200DS, but proprtionally
larger (i.e. 254 mm diameter). I have only a single photograph showing
this type, and it appears to have been completely unpainted; thus, the
appearance here.
Limited manufacture of the BRAB-500DS was undertaken during
1940-41. The munition had seemed to be impressive, but testing at the TTT
revealed that it was not particularly accurate, and plans to produce this
bomb in large numbers were abandoned. Something like 500 examples were
built in all, of which 136 examples were delivered to the Army (including
the LVO and KOVO). Their subsequent employment during the GPW is not clear
at this time.
BETAB-750DS 1941
Length: 4000 mm
Max. Diameter: 305 mm
Overall Weight: 766.3 kg
Weight of Explosive Filling: 74.3 kg |
 |
If the BRAB-500DS seemed a bit over-sized, the BETAB-750DS
was a colossus. The sheer impracticality of employing a four meter long
bomb munition would seem to have been obvious to anyone, but apparently
this was not the case at the NII-24. Constructed as the previous rocket
bomb types, the diameter of this weapon was 305 mm, both the rocket housing
and the warhead. It is shown here in IMP finish.
Only a small number of -750DS bombs were built, these
mostly of an experimental nature, and during 1940-41 eighty were completed.
Following the failure of the BRAB-500DS at the TTT, all plans to pursue
this weapon seem to have come to an end.
However, despite this premature termination, all of the
BETAB-750DS munitions were delivered to the Baltic Fleet (KBF) during 1941.
The KBF, remarkably, retained and subsequently utilized these weapons during
the War, and indeed more than once with notable success. The -750DS could
only be carried by the Il-4, two at a time. On the other hand, the impact
of this mighty AP bomb must have been tremendous, and several of the stubborn
concrete bunker emplacements in the Gulf of Finland were apparently destroyed
by these weapons.
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