PAK-FA [T-50] Latest Armaments
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Transcript of PAK-FA [T-50] Latest Armaments
ADVANCED WEAPONSADVANCED WEAPONS FOR ADVANCED WARPLANESFOR ADVANCED WARPLANES
Development of a new generation of precision guided munitions is nearing completion
Peter STONE
Yevg
eny Y
ero
khin
m i l i t a r y a v i a t i o n | w e a p o n s
Late January 2010 saw the maiden flight of the Sukhoi PAK FA Future Tactical
Aircraft. In one of his interviews, Boris Obnosov, Director General of the Tactical
Missiles corporation, the key supplier of weapons for the fifth-generation
fighter, said that the development of air-launched weapons for the aircraft were
on schedule. The corporation is completing the development of 14 types of
advanced missiles and smart bombs spanning virtually the whole spectrum of
air-launched weapons. The emphasis has been placed on air-to-air and air-to-
surface guided missiles.
New air-to-air missiles on’s enhanced powerplant and combined aero-
The latest air-to-air missiles under develop- gas-dynamic controls enable the RVV-MD
ment include short-, medium- and long-range to use higher angles of attack than the R-73E
ones and are being developed by the Vympel can, with the former’s target designation angles
design bureau, a Tactical Missiles subsidiary. ranging ±60 degrees. It also can eliminate
The RVV-MD short-range air-to-air mis- threats manoevring at as much as 12 g.
sile is designed for use by fighters, attack The highly lethal RVV-SD medium-range
aircraft and combat helicopters. The cutting- missile is intended to deal with aerial threats,
edge missile, fitted with an upgraded all-aspect e.g. hostile fighters, attack aircraft, bomb-
two-mode heat-seeking head, features a 30% ers, airlifters, helicopters and cruise missiles.
increase in the range over the R-73E dogfight Compared with the RVV-AE missile, the
missile it is designed to replace. The new weap- RVV-SD features a big increase in maximal
RVV-MD and RVV-SD AAMs
range – up to 110 km. The RVV-SD kills tar-
gets jinking at up to 12 g at any time of day and
night, attacking them from any aspect in the
face of electronic countermeasures (ECM) in
the look-down mode, including the multiple-
target launch-and-leave attack capability.
Air-to-ground missiles
The design of the latest AGMs is heavily
modularised. The approach has been embod-
ied in the advanced Kh-38ME multi-purpose
missile able to mount a number of combined
guidance packages, including the inertial
guidance system and terminal precision-guid-
ance package variants wrapped around laser,
thermal-imaging and radar or satnav homing
heads. The missile can pack a formidable blast/
fragmentation or penetrator warhead, with
a cluster-type warhead being an option. The
dual-pulse solid-fuel rocket motor develops
a velocity exceeding the sonic speed by more
than twice.
Table 1 offers a comparison of the basic
characteristics of the Kh-38ME and the
widely-known previous-generation Kh-25M
AGM (the data pertaining to the Kh-38MLE
and Kh-25ML laser beam-riding missiles).
According to the table, the Kh-38MLE is
virtually four times more effective than the
Kh-25ML in terms of maximum range and
warhead weight.Yevg
en
y Y
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kh
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30 take-off july 2010 w w w . t a ke - o f f . r u
m i l i t a r y a v i a t i o n | w e a p o n s Y
evg
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kh
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Yevg
eny Y
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Kh-38ME
The Kh-59MK2 air-to-ground missile
has been developed to deal with a wide spec-
trum of stationary ground targets. It is effec-
tive against targets with the known grids,
including the targets lacking the radar, IR
and optical signatures. The missile is a fire-
and-forget weapon using the autonomous
recognition of the terrain adjacent to the
target. The Kh-59MK2’s enhanced range
accounts for 285 km and its formidable
penetrator or cluster-type warhead has been
increased up to 320 kg and 283 kg respec-
tively.
The Ovod-ME multi-purpose missile sys-
tem wrapped around the Kh-59M2E guided
missile eliminates surface targets identified
visually by the weapon systems officer on
the multifunctional display. The Kh-59M2E
missile-based Ovod-ME system has the
round-the-clock capability, including the
ability to kill targets in low visibility.
Multirole PGMs also include guided bombs.
The offer to foreign customers includes a whole
series of smart bombs furnished with satellite
navigation and laser beam-riding capabilities.
Antiradiation and antiship missiles
More advanced antiradiation and antiship mis-
siles, Kh-31PD and Kh-31AD respectively, are
being derived from the high-velocity Kh-31P/A
missiles fitted with a combined powerplant of a
ramjet sustainer and a solid-fuel booster motor.
The advanced missiles of the type are far superior
to the similar-purpose missiles of the previous
generation in terms of performance. See Table 2
for the comparison of the characteristics of the
export versions of the Kh-31-family weapons.
The new-generation Kh-31PD/AD missiles
are equipped with more accurate cutting-edge
guidance systems and feature a two-plus times
increase in range and a warhead lethality hike of
at least 15–20% over the previous models.
Table 2. Basic characteris
Launch weight, kg
tics of high-veloKh-31AD
715
city antiship and Kh-31A
610
antiradiation misKh-31PD
715
siles of the Kh-3Kh-31PK
605±10
1 family Kh-31P
600
Warhead weight, kg 110 94 110 88±2,5 87,5±2,5
Maximum range from H=15,000 m,
M=1.5, km 120–160 70 180–250 up to 110 up 110
Missile maximum (average) velocity,
m/s >1,000
1,000
(600–700) >1,000
1,000
(720–750)
1,000
(600–700)
Guidance system inertial + active
radar homing
autopilot + active
radar homing
inertial +
wideband passive
radar homing
interchangeable
passive radar
homers
interchangeable
passive radar
homers
Table 1. Basic characteristics of general-purpose air-to-ground missiles
Kh-38MLE Kh-25ML Missile launch
weight, kg up to 520 299±8
Warhead weight, kg up to 250 86
Range, km
- from H=50 m
- from H=5,000 m 3–40
3–10
8–10
Launch altitude
bracket, m 200–12,000 50–5,000
Guidance system
inertial + semi-
active laser beam-
riding
semi-active laser
beam-riding
The evolution of subsonic sea-skimming anti-
ship missiles has embodied in the Kh-35UE
missile featuring considerable aerodynamics
and powerplant improvements and more capa-
ble guidance and control systems compared
with the previous-generation Kh-35E antiship
missile. Refer to Table 3 for a comparison of the
characteristics of the advanced Kh-35UE anti-
ship missile and its predecessor Kh-35E.
The new missile features a twofold increase
in the maximum range. Its combined guidance
system reliant on the inertial-guidance satnav
active/passive radar homing capabilities allows
the Kh-35UE a higher degree of precision and
countermeasures immunity and a wider spec-
trum of targets it can take out, including those it
can kill in the face of ECM. The target acquisi-
tion range of the advanced missile has more than
doubled, with the Kh-35UE having the same
dimensions the Kh-35E has, which makes them
interchangeable.
Developing and producing the new generation
of PGMs calls for a design and technology level
drastically different to that inherited from the
previous century. The Tactical Missiles corpora-
tion is running a purposeful gradual upgrade of
its technological capabilities to this end. At pres-
ent, the corporation is running 17 programmes
on updating and reconstructing its production
capabilities. This enabled it to launch a series
of development efforts on sophisticated PGMs.
Special attention is being paid to refining the
ground test facilities to enable them to ensure
a high degree of sophistication of development
work, thus slashing the number of flight tests.
The work is currently right on schedule.
Table 3. Basic characteristics of subsonic antiship missiles of the Kh-35 family
Kh-35UE Kh-35E Launch weight, kg
- plane-launched missile
- helicopter-launched missile
550
650
~520
~610
Warhead weight, kg 145 145
Range bracket, km 7–260 5–130
Sea-skimming altitude, m:
- cruising leg
- terminal leg
10–15
4
10–15
~4
Velocity (Mach) 0.8–0.85 ~0.8
Max post-launch horizontal turn
angle, deg. ±130 ±90
Guidance system
inertial +
satnav +
active/passive
radar homing
inertial +
active radar
homing
Homing head’s maximum target
acquisition and lock-on range, km 50 >20
Kh-35UE
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