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  1. MBT Arjun Tank

    … by CVRDE during the development of MBT Arjun are in Engine, Transmission, Hydropneumatic Suspension, Hull and … Ammunition Mobility High performance engine Robust and effective transmission system … : 40 km/hr Ground pressure : 0.84 kg/sq. cm. Engine power : 1400 HP at 2400 rpm Engine

  2. Aeromechanical Systems

    … High speed / High precision bearings for Small Turbo Fan Engine CVRDE Gear Box Aircraft … Aircrafts CVRDE Lube filters for Aero Engine CVRDE Landing Gear …

  3. Click here to check the final Result of (0301- junior Translation Officer (JTO)) and (1001-fire Engine Driver 'A')

    … of (0301- junior Translation Officer (JTO)) and (1001-fire Engine Driver 'A') 479 views …

  4. नया पंखा

    … imposes very high inlet pressure distortion at the engine inlet. The fan being the first component in a gas turbine engine is subjected to this high inlet distortion which …

  5. C4ISR

    … Unit for  Infra Red Search & Track (IRST) of Twin Engine Deck Based Fighter IRDE Sensor Head Unit for Infra Red Search & Track (IRST) of Twin Engine Deck Based Fighter IRDE Advanced …

  6. Power Take Off shaft of LCA Tejas

    … Power Take Off (PTO) Shaft for LCA Tejas couples the Engine mounted accessory gear box with Aircraft mounted … (PTO) shaft for flight fitment. Successfully completed Engine ground run Test and LSTT in LCA-Tejas. ToT imparted …

  7. Aerospace Resources Panel

    … overhaul/ maintenance of military & civil aircraft, engine & systems Panel formulates strategies and plans with … overhaul/ maintenance of military & civil aircraft, engine & systems Panel formulates strategies and plans with …

  8. छोटा टर्बो फैन इंजन

    … Small Turbo Fan Engine is aimed for Unmanned Aerial Vehicle applications. It is a twin spool engine without afterburner. It has autonomous starting …

  9. Kaveri Marine Gas Turbine

    … Kaveri Marine Gas Turbine engine is a derivative of Kaveri engine developed for Naval ship propulsion. Gas turbine when …

  10. New Fan

    … imposes very high inlet pressure distortion at the engine inlet. The fan being the first component in a gas turbine engine is subjected to this high inlet distortion which …

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