Rao, KVL and Chidananda, MS and Venkatesh, S and Jagannatha Rao, B and Shyamsundar , SR and Krishna Kumar, VS (1986) Studies on Combustion of Polymeric Fuel with Secondary Air Injection. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Mixed propulsion system is a novel concept of propulsion and has therefore been a subject matter of renewed studies in recent times. This concept has brought out new problems which do not find ready answers in the conventional technology of air-breathing propulsion systems. Therefore, it was proposed to undertake experimental studies related to the design and development of a scaled down version of a mixed propulsion system in collaboration with the Defence Research and Development Laboratory, Hyderabad. As part of these studies, a test facility was built for carrying out tests on related combustor systems with simulation of inlet conditions. The test facility consisted of a single axis (horizontal) thrust stand, capable of measuring thrusts upto 300 kgf along with the associated instrumentation.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Integral Rocket-Ramjet, Ramjet, Polymeric fuel |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Propulsion Division, Propulsion Division, Advanced Composites Division, Propulsion Division, Propulsion Division, Propulsion Division |
| Depositing User: | Ms Indrani V |
| Date Deposited: | 22 Aug 2012 09:52 |
| Last Modified: | 22 Aug 2012 09:52 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10829 |
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