Altitude Performance of a Turbojet Engine Using Pentaborane Fuel
Description:
Memorandum presenting a turbojet engine with a two-stage turbine operated with pentaborane fuel continuously for 11.5 minutes at a simulated altitude of 55,000 feet at a flight Mach number of 0.8. The engine incorporated an NACA combustor designed specifically for use with pentaborane fuel. Results regarding oxide formation and deposition, engine operating point, effect of oxide deposits on component performance, effect of oxide deposition on overall performance, and some operational comments a…
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Date:
May 20, 1957
Creator:
Sivo, Joseph N.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department