An Investigation of the Application of the Gas Generator-Free Turbine Cycle to a Nuclear Powered Aircraft
Description:
This study has investigated the feasibility of installing a gas generator-free turbine type power plant in the R3Y aircraft, using a circulating fuel reactor as a power source. Two variations of the cycle were considered. The split flow cycle bleeds high temperature, high pressure air from the gas generator directly to the free turbine in the wing. The through flow cycle partially expands the high temperature, high pressure air through the compressor turbine of the gas generator then directs th…
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Date:
August 1, 1957
Creator:
Alvis, J. H. & Chessman, S. R.
Item Type:
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Partner:
UNT Libraries Government Documents Department