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HAL TEZAS MK 2

TEZAS MK2 FIGHTER JET

TEZAS MK2 IS LIGHTEST SUPERSONIC AIRCRAFT OF ANY OF IT’S TYPE IN THE ENTIRE WORLD. HAL TEZAS MK2 IS INDIA MADE SINGLE ENGINE, DELTA WING, LIGHT FIGHTER JET. TEZAS MK2 FIGHTER JET WAS DESIGNED BY INDIAN AERONAUTICAL DEVELOPMENT AGENCY (ADA) AND HINDUSTAN AERONAUTICS LIMITED (HAL). TEZAS MK2 FIGHTER JET IS LIGHT COMBAT AIRCRAFT DESIGNED FOR INDIAN AIR FORCE.

THIS WAS THE FIRST TIME INDIA SUCCESSFULLY DESIGNED DIGITAL FLY-BY-WIRE (FBW) FLIGHT CONTROL SYSTEM. TEJAS IS EQUIPPED WITH TAIL LESS COMPOUND DELTA WING CONFIGURATION WITH A SINGLE DORSAL FIN. THE TEZAS MK2 IS ALSO KNOWN AS LIGHT COMBAT AIRCRAFT (LCA) BECAUSE FIGHTER JET WAS DEVELOPED UNDER LCA PROGRAM.

LIGHT COMBAT AIRCRAFT IS DEVELOPMENT PROGRAM CONDUCTED BY INDIAN AERONAUTICAL DEVELOPMENT AGENCY (ADA) AND HINDUSTAN AERONAUTICS LIMITED (HAL). TEZAS MK2 IS CLASSIFIED AS SUPERSONIC LIGHT COMBAT AIRCRAFT. TEZAS MK2 IS ALSO SECOND SUPERSONIC FIGHTER JET DEVELOPED BY INDIAN BY HINDUSTAN AERONAUTICS LIMITED (HAL). THE PRINCIPLE AND MOST OBVIOUS GOAL OF TEZAS MK2 FIGHTER JET IS TO REPLACE INDIA’S AGEING MIG-21 FIGHTER JET.

FEATURES:

(A) SUPERSONIC AT ALL ALTITUDES
(B) 15 KM SERVICE ALTITUDE
(C) TAILLESS, COMPOUND DELTA WING
(D) COMPOSITE STRUCTURE
(E) IMPROVED PERFORMANCE
(F) IMPROVED MAINTAINABILITY
(G) IMPROVED SURVIVABILITY
(H) DIGITAL FLY BY WIRE
(I) FUEL DUMP SYSTEM
(J) MULTI-MODE RADAR

 

UPGRADES:

(A) HIGH THRUST ENGINE

(B) STRUCTURAL WEIGHT REDUCTION

(C) AERODYNAMIC IMPROVEMENT

(D) UPGRADED FLIGHT CONTROL SYSTEM

(E) ELECTRONIC WARFARE SUIT

(J) AVIONICS UPGRADE

(H) IN FLIGHT REFUELING SYSTEM

(I) ONBOARD O2 GENERATION

(J) INCREASED FUEL CAPACITY

 

AIRFRAME:

(A) ALUMINUM- LITHIUM ALLOYS
(B) CARBON-FIBRE COMPOSITES
(C) TITANIUM ALLOYS

PERFORMANCE:

(A) MAXIMUM SPEED: Mach 1.8
(B) RANGE: 850 km
(C) COMBAT RANGE: 500 km
(D) FERRY RANGE: 1,750 km
(E) SERVICE CEILING: 15,000 m
(F) WING LOADING: 55.2 kg/m2
(G)THRUST/WEIGHT: 0.94

PROPULSION:

(A) GENERAL ELECTRIC F404-GE-F2J3 AFTERBURNING TURBOFAN ENGINE

 

HAL LIGHT COMBAT AIRCRAFT TEZAS MK2 PRODUCTION PARTNERS:

(A) FRONT FUSELAGE: DYNAMIC TECHNOLOGIES LTD. BENGALURU
(B) CENTER FUSELAGE: VEM TECHNOLOGIES HYDERABAD
(C) REAR FUSELAGE: ALPHA TOCOL BENGALURU
(D) WINGS: LARSEN & TOUBRO COIMBATORE
(E) TAIL FIN AND RUDDER: NATIONAL AEROSPACE LABORATORY AND TATA ADVANCED MATERIALS LTD

ASSEMBLED AT: HINDUSTAN AERONAUTICS LIMITED BENGALURU

SPECIFICATION:

(A) CREW: 1
(B) LENGTH: 13.2 M
(C) WINGSPAN: 8.2 M
(D) HEIGHT: 4.4 m
(E) WING AREA: 38.4 m2
(F) EMPTY WEIGHT: 6,560 kg
(G) GROSS WEIGHT: 9,800 kg
(H) MAX TAKE OF WEIGHT: 13,300 kg
(I) FUEL CAPACITY: 2,458 kg
(J) PAYLOAD: 3,500 kg
(K) JET ENGINE: GENERAL ELECTRIC F404-GE-F2J3 AFTERBURNING TURBOFAN ENGINE

ARMAMENT:

(A) ROCKET: S8 ROCKET PODS
(B) MISSILES: AIR TO AIR, AIR TO SURFACE, AND ANTI-SHIP.
(C) BOMBS: LASER GUIDED, GLIDE BOMB, AND CLUSTER WEAPON.

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