Strana 15
Specifications:
Length: 2095mm
Diameter: 120mm
Span: 390mm
Weight: 43.5kg
Warhead: 3kg
Service Life: 40 Flight Hours
or 40 Landings
APU-62 IIM Components
1. Lower Pylon
2. Side Pylon
3. Forward Aerodynamic Cover
4. Side Cover
5. Rear Aerodynamic Cover
6. Front Stop
7. Rear Stop
8. Mounting Eye
9. Mounting Lug
10. Arming Pin with RBF Tag
TECHNICS / EQUIPMENT
Infrared seeker head with destabilizers, to which is attached the warhead
(between the destabilizers and rudders) of the R-60M missile.
Control section of the R-60M missile, a view of the lower front
part with the four control fins, the ‘U
-
B’ switch and concealed
electrical wiring and piping on the outer surface of the missile.
Twin APU-62 IIM (APU-60-IIM) launcher.
Main Components:
Infrared seeker head with destabilizers
(1) – serves to capture and track a thermally
contrasting target, is of a passive type (only
receives reflected energy from the target,
does not emit anything itself), and is equipped
with a simple, uncooled seeker. It detects and
identifies the target, transmits a signal about
its capture to the APU launch rail, measures
the angular velocity of the target and generates
control signals for guiding the missile in flight.
The warhead (2) is of the high-explosive type,
equipped with a non-contact radar proximity
fuse and a detonation mechanism.
Control section (3) – contains an impact
sensor that sends an electrical impulse to
the detonation mechanism when the missile
directly hits the target, it also contains autopilot
blocks, automation blocks and a power supply
voltage stabilizer and a connecting cable
(for missile-launcher-aircraft communication).
The control section also contains rudders
(which change the missile's flight trajectory)
and the ‘U
-
B’ switch, the position of which
determines whether the missile is in combat or
combat training mode.
Power section (4) – here are located the PAD
pressure accumulator among other devices,
a proximity radar detonator (green antennas,
rectangular in shape) and a missile launch
indicator (5).
Rocket motor with solid propellant is the
source of propulsion that carries the missile
to the target. The motor body also houses the
missile suspension nodes for the launcher and
fins complete with rollerons.
INFO Eduard
15
May 2025