Question
The following requirements are given for a solid propellant rocket motor: Sea level thrust: 740 lbf average Duration: 42 sec. Chamber Pressure: 750 psia Operating
The following requirements are given for a solid propellant rocket motor: Sea level thrust: 740 lbf average Duration: 42 sec. Chamber Pressure: 750 psia Operating Temp.: 70 F Propellant: Ammonium Nitrate-hydrocarbon Determine Isp, throat and exit areas, flow rate, total propellant weight, total impulse, burning area and mass.
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Step: 1
Properties for given propellant Ammonium Nitrate hydrocarbon are K 126 T 1 2700F or 3160k R 0010 ins...
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Step: 2
Step: 3
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Principles of heat transfer
Authors: Frank Kreith, Raj M. Manglik, Mark S. Bohn
7th Edition
495667706, 978-0495667704
