Brief Studies of Turbojet Combustor and Fuel-System Operation With Hydrogen Fuel at -400 Degrees F
Description:
Memorandum presenting a single J33 combustor and an experimental tubular combustor incorporating a fuel vaporizer as operated with gaseous hydrogen at temperatures slightly above the boiling point of the fuel. Data were obtained to explore possible effects of the fuel temperature on combustor performance and on the control and measurement of fuel flow.
Date:
March 7, 1957
Creator:
Straight, David M.; Smith, Arthur L. & Christenson, Harold H.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department