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Specific Air Range & Specific Endurance
Key cruise parameters are Range (distance flown) and Endurance (time of flight). It is important to be able to relate these to the amount of fuel burned; in particular, it may be desirable to maximize the range or the endurance for a given quantity of fuel. Specific Air Range (SAR) = distance flown per unit fuel burned Specific Endurance (SE) = time of flight per unit fuel burned Drag, power, functions of weight, which reduces during cruise due to fuel burn SAR and SE are therefore point performance parameters Need to integrate SAR and SE over cruise to determine range and endurance
Re-Heat Nozzles : If re-heat was fitted to an engine with a standard sized fixed area propelling nozzle, the expansion of gases caused by the use of re-heat would increase the
Specific Air Range & Specific Endurance Key cruise parameters are Range (distance flown) and Endurance (time of flight). It is important to be able to relate these to the amou
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