Avionics Division Hyderabad
IFF 1410AIdentification of friend or Foe, automatic replies to ground or airborne interrogatorsModular ConstructionPower output >350W (24.5 dBw) PEAK. Availability of large no. of codes ,secure mode
IFF MKXII Transponder 2420ATo identify reliably the aircraft of interest as friendly or foe automatic replies to ground/ airborne interrogators.- Dual channel digital receiver for DPSK demodulation.
- TCAS interface.
- Security features for encryptor and decryptor provided in Crypto unit.
- System specifications as per STANAG 4193 and ICAO Annex-10.
- Solid- state 350W transmitter.
INCOM -1210AIntegrated Radio Communication SystemV/UHF Comm in Aero and Marine range with ECCM FacilityCommunication in AM/FM/Data/ECCM Mode
ACS 235Advanced Radio communication systemCommunication In Normal / Secure & Voice / Data Modes With ECCM (FH & DSSS) Features. ½ ATR Dimension. MIL-STD-1553B Data Bus Compatibility.Frequency:30-407 MHz Sensitivity: SINAD NLT 10 dB @ 2 µV Tx Power :10 Watts in AM, 15 watts in FM. Channel Spacing : 25 KHz, 12.5 KHz & 8.33 KHz.
COM 1150AUHF Standby equipmentHybridized version10 Preset Channels
Mission Computer (MC)Navigation & Guidance; Weapon Aiming – Task Management etc.Multi - processor system with parallel processing capabilityCPU-486, 1553B, ARINC- 429 Discrete Input / Output
Display Processor (DP)Display Management & Control of MFDs & HUDMulti- processor system with parallel processing capabilityCPU-486, 1553B, Color and Monochrome signal generation.
Radar Computer- 1 Radar Computer- 2 (RC1 & RC2)Interface to MC, Radar control parameter computation.Multi- processor system with parallel processing capabilityCPU -486, 1553B, ARINC- 429 Discrete Input / Output, High speed 18 bit parallel data Bus.
RAM 1701ARadio Altimeter for height indication over terrainFully Indigenously designed and developed by HAL Hyderabad Modular ConstructionMIL-STD-1553B Data Bus Compatible
1 kW HF TransmitterHF system for use between ship to ship, ship to shore, shore to shore communicationRemote control capability Automatic Link EstablishmentRF power O/P: 1 kW±1 dB PEP Harmonic attenuation: 55dB PEP (typical).
5 kW HF TransmitterA Solid State transmitter operating in the High frequency Band and meant for use between Shore to Ship, Shore to Shore communicationDirect Digital Synthesis, Remote control Capability, Automatic link Establishment, Capacity to operate in a co-located environment.RF Power O/P: 5000W±1 dB Frequency Range: 1.5 to 30 MHz with capability to select in steps of the 1 Hz.
PAR (Precision Approach Radar)Provides Azimuth, elevation, bearing information to the AircraftX–Band (9–9.2GHz)Range: 30 Km
TACANTactical Air Navigation System, Provides magnetic beaming, slant distance information, Beacon identification tone and run way approach.Fully Indigenously designed and developed by HAL Hyderabad Modular ConstructionRange Accuracy: ±0.1NM
Range Capability: 300NM
Beaming Accuracy: ±10
Receiver Sensitivity: -90dBm
VOR/ILSVHF omni Range/ Instrument landing system, Used for route navigation, runway approach and landing.Fully Indigenously designed and developed by HAL Hyderabad. Modular ConstructionAccuracy: ±3degree, Sensitivity:
= - 99 dBm (VOR/LOC)
= - 87 dBm (GS)
SSDVRSSolid State Digital Video Recording System to record the video picture and flight data in Digital format.Supports multiple video standards and formats.MIL-STD 1553B interface. Provision for Airborne Replay.
RLSU RADARPrimary sensor for Su-30 to detect and track Airborne, Ground and Sea targets.Passive Phased Array RadarTracks upto 16 fighters in an area of 50 km X 50 km, locks 4 & targets 2 fighters at a time
Voice Warning SystemIntended for automatic warning of crew members with emergency, preventive and informative messagesLicensed Avionics for Su-30Signals in the form of sequential code on ARINC 429. Maximum number of playback messages – 256
Weapon Control SystemPreparation of Aircraft armament to combat applicationsGuided tracking of missiles till it hits the targetEmergency start-up
Fire Alarm SystemProvides audio and visual alarm indication to the pilot in the event of fire or over heat in the engine compartmentsLicensed Avionics for Su-30The flame temperature is about 1100°C.
Communication Means ComplexEnsures two-way telephone communication in V/UHF and HF rangesUses Spread Spectrum technique Modular constructionHF range (2.0 – 23.9999) MHz with 100 Hz spacing VHF range (100.000 – 149.975) MHz UHF range (156.000 – 173.975) MHz with 25 kHz spacing.