| || Effect of Fuel Properties on the Specific Thrust of a Ramjet Engine
Author : Gany, Alon
Source : Defence Science Journal ; Vol:56(3) ; 2006 ; pp 321-328
Subject : 621.1 Engines;629.7 Aeronautics;629.76 Rockets and Missiles
Keywords : Ramjet engine;Specific thrust;Specific impulse;Ramjet propulsion;Fuel-air ratio;Specific heat release;Fuels;Fuel efficiency;Fuel rich propellant
Abstract : Various aspects of specific thrust in ramjet propulsion have been considered. It is shown that while the peak specific impulse of ideal ramjet is theoretically obtained for fuel/air ratio f 0, the specific thrust which determines the thrust level of a given engine at certain operating conditions, increases with increasing fuel/air ratio up to (approximately) the stoichiometric ratio. Furthermore, in general, the specific thrust is related to the heat release per unit mass of air fqR, where the theoretical maximum is approximately proportional to its square root in stoichiometric conditions, fstqR. This can be the basis for selecting an appropriate fuel according to its potential specific thrust. It should be noted that certain metals such as magnesium, aluminum, and zirconium can provide about three-times higher specific heat release than hydrocarbons or hydrogen. Thus, these may be the better candidates for missions requiring high specific thrusts.