A ramjet drives a missile at V0=966m/s at an altitude of 33.5km (air density 0.01kg/m3 and T0=232K). If the missile inlet captures a stream tube of air A0=1,1m2 in area, the fuel-to-air ratio is 0,049, and the fuel heating value is 50MJ/kg.if the ramjet engine produces net thrust Fn= 8,9 kN , What is the useful power that the engine introduces to the missile?

The missile speed, Vo = 966 m/sThe density of air = 0.01 kg/m^3The temperature, To = 232 KThe…

Answered: A ramjet drives a missile at V0=966m/s…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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A ramjet drives a missile at V₀=966m/s at an altitude of 33.5km (air density 0.01kg/m³ and T₀=232K). If the missile inlet captures a stream tube of air A₀=1,1m² in area, the fuel-to-air ratio is 0,049, and the fuel heating value is 50MJ/kg.

if the ramjet engine produces net thrust F_n= 8,9 kN ,

What is the useful power that the engine introduces to the missile?

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