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By T.S. Subramanian
CHENNAI, FEB. 29. The Indian Space Research Organisation is working on air-breathing rocket engines that will use hydrogen as fuel and the air from the atmosphere as the oxidiser to burn that hydrogen. This is a frontier technology, especially because it involves the use of hydrogen a clean source of fuel. The ISRO Chairman, G. Madhavan Nair, told The Hindu: "We have initiated work on air-breathing rocket-propulsion systems. They will use hydrogen as fuel and air as the oxidiser. One of the engines for this mission has been conceived." Plans are under way to conduct tests of this engine. "In another three months, we will be able to show some results. If we have a good result, it will be a breakthrough. We are really considering to hold the flame at Mach 6," he said. Mach 6 is six times the speed of sound that travels at 1,100 km an hour. All conventional aircraft engines are air-breathing. They carry fuel (aviation kerosene) with them, and take in the air from the atmosphere as oxidiser to burn the fuel. They can do this because the aircraft fly in the earth's atmosphere. For a rocket (a launch vehicle), which travels much beyond, there is no atmospheric air. The rockets carry oxygen, for example, in the form of ammonium perchlorate for burning the fuel in a solid propellant. But when an air-breathing rocket propulsion system flies within the atmosphere, it sucks in the oxygen from the atmosphere for burning the fuel and does not have to carry an oxidiser separately. Mr. Nair said: "The air-breathing rocket propulsion systems basically collect air from the atmosphere. As they do that, the drag increases considerably. Then, using this air, we are burning the hydrogen. So the thrust we have to develop should be more than the drag. This is really a million-dollar question, especially in hypersonic regime. I don't think many people have solved this. We are trying to make a start in this field and some experiments in the next few months will give us a feel of this problem. We are really considering to hold the flame at Mach 6.
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