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Calculate the ideal density specific impulse in units of kgsecm3 for the propellant combination LOX HTPB at an oxidizer to fuel ratio of 2 3 at a pressure ratio across the nozzle of

Calculate the ideal density-specific impulse (in units of kg-sec/m3) for the propellant combination LOX/HTPB at an oxidizer-to-fuel ratio of 2.3 at a pressure ratio across the nozzle of 1000/14.7 and an optimum expansion. Use the information in Table 16–2 and a fuel density of 920 kg/m3. Compare your result with the value of LOX/RP-1 bipropellant listed in Table 5–5.

 

 

 

Jul 23 2020 View more View Less

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