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INTRODUCTION TO LIQUID PROPELLANT ROCKET ENGINES
ROCKET ENGINE DESIGN IMPLEMENTS
INTRODUCTION TO SAMPLE CALCULATIONS
9 other sections not shown
A-l stage engine absolute flow actuator alloy applications axial axial-flow bellows bipropellant centrifugal chamber pressure characteristics coefficient combustion chamber components coolant cooling cryogenic density diameter diaphragm discharge duct effects efficiency engine system equation factor flange flow angle flow rate fluid ft/sec fuel pump gas flow gas pressure regulator gases gimbal helium hydrogen hypergolic ignition impeller rotor inducer stator injector isentropic lb/sec liquid propellant loads main propellant main propellant tanks maximum mixture ratio monopropellant nozzle NPSH operation orifice oxidizer oxidizer pump parameters pellant percent performance pilot valve pres pressure drop propellant flow propellant tank propulsion system psia pump inlet radial rocket engine rotating rotor blades Sample Calculation seal shaft shown in figure specific heat ratio specific impulse specific speed static stator stator vane stress tank pressure temperature throat thrust chamber tion tube turbopump typical vane angle velocity diagrams volute wall weight