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India : A shortfall in performance of Kaveri engine led the DRDO to collaborate with a foreign firm
 
BY : LIVE MINT

Nearly 20 years after it promised an indigenous engine to power India’s light combat aircraft Tejas, the Gas Turbine Research Establishment, or GTRE, the country’s sole aero engine design house, is now seeking outside help.
It has chosen French aircraft engine maker Snecma SA to jointly build an engine to replace Kaveri, a project named after the river in southern India. T. Mohana Rao, director of GTRE, a unit of the Defence Research and Development Organisation, explains why it had to choose a partner and talks about the future of the Kaveri programme. Edited Excerpts:

What is the status of the Kaveri engine development project?

We have a functional engine, but there is a slight shortfall in performance. It has achieved dry thrust of 4,600kg and reheat thrust of 7,000kg in Bangalore, which is around 3,000ft above sea level. So, it would be around 5,000kg dry thrust and 7,500kg reheat thrust at sea level. The engine is short of thrust by 400kg and overweight by around 150kg. Also, we still have to perform long- endurance tests of the engine to run for many hours.
Does this mean the engine for the light combat aircraft would be further delayed?
In aircraft engine development, particularly when you are doing it for the first time, you cannot set a timeline. We could take five or six years. The Indian Air Force (IAF) cannot wait for an engine for that long, and the government said if there is any engine house that we can partner, we could go ahead and do a joint venture on risk-sharing basis.
Only NPO Saturn and Snecma responded of the five. General Electric Co., Rolls-Royce Plc. and Pratt and Whitney declined. Nearly two-and-a-half years after we started the process, we have identified Snecma. The government told us to consult IAF and decide on the air staff requirements before we sign a contract.
Has Snecma given a timeline for the new engine?
Snecma will bring its (engine) core that is named Eco. A core, which comprise a compressor, combustor and high-pressure turbine, is the heart of any jet engine. The engine will have less weight and more reheat thrust along with certain other changes to meet the original design intent. They will have a workshare of 45%, and ours would be 55%. Nearly 85% of the manufacturing would be within the country. The engine would be certified for fitting in the aircraft in around four years. Hindustan Aeronautics Ltd will produce the engine and all future aircraft engines in India would be from the joint venture.
But why so late? Couldn’t you have gone for a global partner much earlier and avoided delays?
It was a decision by the government. When Kaveri was conceived, India did not have a design base for aero engines, except for some work we had done earlier. Globally, they first pick an engine and then build the aircraft. Here, we decided that by the time the light combat aircraft was ready, we should have our own engine. The engine (supplied by General Electric) currently powering the aircraft is inferior to Kaveri’s specifications.
IAF wanted us to build a highly stable engine with a digital computer to control it, and a two-lane manual reversion (a backup for the first time in the world). Rolls-Royce and GE validated our design. Now we have a design base, huge infrastructure and talent pool in engines. We could not have built this if we had not taken up this project.
What will happen to Kaveri and the work you have done?
The core of Kaveri is performing well. Because of the lower thrust, it cannot be used on combat aircraft. It can be used to power unmanned combat aerial vehicles. We have already demonstrated a marine version of Kaveri using diesel as fuel for the Indian navy. It can also be used as a large 12MW industrial genset for power generation.
 
 
 
   
 
 
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  •  
     
    Comments (3)  Print
     
     
    #1 Author: pq (21 August 2008 01:21)
     
    the author is nnot telling the whole truth. why is kaveri overweight? is it because hal has not developed hiogh-temp lightweight titanium alloys for compressor and turbine blades? or is it because more stages are being used in the engine to build up requisite pressure of the input air to the combustion chamber?

    why can't hal engineers copy a russian or a usa design? why doesn't hal design an airframe for tejas to incorporate two engines instead of one?

    spill the beans.
     
     
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    #2 Author: Aswini (31 August 2008 23:57)
     
    Sir
    if somebody can convey this to Mr T MOHAN RAO (director GTRE). From the Publicly available information, that I have gathered, I understand they have a target thrust of 20000 lbs but have been able to achieve some 18000 lbs+ consistent thrust. The engine is failing high altitude tests (that’s all is publically available)
    I have a suggestion to make.
    There is a lot of publically available information on Toroidal aerospike rocket motor design. The information must be investigated upon for the design of the kaveri engine
    The information might be significantly helpful, to deal with variation in fluctuation of ambient atmospheric pressure & effectively manage the stress on the internal components of the engine
    Thank you



     
     
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    #3 Author: avatar_singh (8 September 2008 16:36)
     
    http://www.larouchepac.com/news/2008/09/05/larouche-u-s-india-nuclear-deal-disaster.html


    LaRouche: U.S.-India Nuclear Deal Is A Disaster
    Increase Decrease

    September 5, 2008 (LPAC)--Lyndon LaRouche today called for the U.S.-India nuclear deal to be scrapped, regardless of the outcome of the Nuclear Suppliers Group meeting, and regardless of whether or not it results in the fall of the Singh government in India. LaRouche reiterated his longstanding view that India's future depends on the full development of its thorium-cycle nuclear power capacity. "The U.S.-India deal, insofar as it prevents the full exploitation by India of the thorium fuel cycle, is, in reality an anti-nuclear deal. It was a rotten deal from the outset, and it should be set aside, regardless of the short-term political consequences in India or the United States,'' LaRouche insisted.

    LaRouche insisted that "no nuclear energy cooperation agreement that inhibits India's rapid and full development of its thorium reactors is acceptable. Thus, the U.S.-India deal should be tossed in the garbage can. If there is to be any U.S.-India bilateral agreement, and if the Nuclear Suppliers Group is to ratify such a deal, then it should be in the best interests of both nations, and clearly this agreement, as currently proposed, is very, very bad for India. The thorium cycle is an existential issue for India,'' LaRouche concluded.
     
     
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