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  • 1988,Vol 9,No. 5

    15 May 1988

NOZZLELESS ROCKET MOTOR

1988, 9 (5): 1-7   

THE ADVANCE AND PROSPECT ON GAS DYNAMICS OF SOLID PROPELLANT ROCKET MOTOR

1988, 9 (5): 8-13   

AN EMPIRICAL METHOD FOR PREDICTING THE SPECIFIC IMPULSE OF SOLID ROCKET MOTORS

1988, 9 (5): 14-18   

ANALYSIS OF THE RESPONSES OF A VARIABLE THRUST LIQUID PROPELLANT ROCKET ENGINE WITH CONTROLLABLE INJECTOR AND VENTURI

1988, 9 (5): 19-27   

COMBUSTION PROCESS ANALYSIS IN A LIQUID ROCKET ENGINE

1988, 9 (5): 28-33   

THE INVESTIGATION OF APPLYING THE BARCHANE DUNE VORTEX GENERATOR INTO THE RAMJET

1988, 9 (5): 34-39   

AN EXPERIMENTAL STUDY OF RE-ENTRY DUCT FOR TURBINE

1988, 9 (5): 40-46   

EXPRESSION OF EROSIVE BURNING CHARACTERISTICS OF COMPOSITE PROPELLANT USING κ-ε PARAMETER

1988, 9 (5): 47-51   

CHARACTERISTIC STUDY OF COMBUSTION FOR AMMONIUM PERCHLORATE/NITRAMINE COMPOSITE PROPELLANTS

1988, 9 (5): 52-56   

PROPELLANTS FOR GAS GENERATORS

1988, 9 (5): 57-61   

THE NOMOGRAM OF PRESSURE OFFSET CASTING FOR COMPOSITE SOLID PROPELLANT

1988, 9 (5): 62-65   

APPLICATION OF IBM-PC COMPUTER IN THE MEASURING AND CONTROL SYSTEM OF LRE INJECTOR COLD-FLOW STAND

1988, 9 (5): 66-69