Research on the crack mechanism of high-burning-rate propellant in the solid rocket motor

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Propellants Explos Pyrotech | / 1卷 / 11期

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[1] RESEARCH ON THE CRACK MECHANISM OF HIGH-BURNING-RATE PROPELLANT IN THE SOLID ROCKET MOTOR
WANG, DA
WANG, NF
QIN, GM
PROPELLANTS EXPLOSIVES PYROTECHNICS, 1995, 20 (01) : 11 - 15
[2] Study on combustion properties of new high burning rate propellant in solid rocket motor
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[4] Calculation of pressure in a solid-propellant rocket motor with the use of a real dependence of the solid propellant burning rate on pressure
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[5] Mitigation of irregular burning in a small solid propellant rocket motor
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[8] On the Effectiveness of Using the Real Law of Solid Propellant Burning Rate As a Function of Solid Rocket Motor Pressure
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[9] Numerical investigation of the velocity-coupled response of propellant burning rate in a solid rocket motor
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[10] THE INFLUENCE OF SPHERICAL GRANULAR PROPELLANTS ON THE COMBUSTION PROPERTIES OF HIGH-BURNING-RATE PROPELLANT
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