- Joined
- 27 December 2005
- Messages
- 16,924
- Reaction score
- 21,798
Main Features
Specifications
System is based on uniform engineering solutions and maximum unification with RLSU-30MKI(BARS-30MKI) for Su-30MKI aircraft.
Source:
NIIP Promotional materials from Aero India 2005
Photo (c) B. Harry, acig.org (via email)
- Aiming and homing of missiles with semiactive, active and infrared homing heads, application of uncontrollable weapons and cannon weapons.
- Simultaneous track-while-scan of up to 15 targets and firing at 4 of them in the whole angular zone in discrete tracking mode, retaining the scan capability.
- Tracking of 2 sea targets and homing one guided missile X-31A at mobile or stationary target
- Tracking preliminary target designation for controlled or uncontrolled weapon firing at ground target.
- While in the mode of attacking one surface target, simultaneous detection of air targets and firing at 1 target in a long-range air fight.
- Fighter flying control during multitarget missiles launching in "air-to-air" mode and during missiles application in "air-to-surface" mode.
- The System is adaptable to any kind of MiG-29 fighter
Specifications
- Detection range
- (effective scattering area - 5m2), km............................100-120
- Lock-on range for automatic tracking, km..............................85
- Working frequencies range...................................................X
- Max beam deviation in surveillance, aiming and weapon
application modes, allowing for the aerial correction angle in azimuth,
provided by drive mechanism...............................................±75° - Electronic scanning by phased array - cone with the
vertex of angle of................................................................80° - Correction angle in azimuth by drive..................................±35°
- Bank stabilization..........................................................±120°
- Mean transmitter power, W.............................................1000
- Cooling.................................................................air-to-liquid
- Weight, Kg.....................................................................250
System is based on uniform engineering solutions and maximum unification with RLSU-30MKI(BARS-30MKI) for Su-30MKI aircraft.
Source:
NIIP Promotional materials from Aero India 2005
Photo (c) B. Harry, acig.org (via email)