Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift

Physics of Fluids ◽

10.1063/1.2746042 ◽

2007 ◽

Vol 19 (9) ◽

pp. 094101 ◽

Author(s):

Gary A. Flandro ◽

Sean R. Fischbach ◽

Joseph Majdalani

Keyword(s):

Rocket Motor ◽

Stability Prediction ◽

Pressure Shift ◽

Prediction Limit ◽

Mean Pressure ◽

Limit Amplitude

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Nonlinear Rocket Motor Stability Prediction: Limit Amplitude, Triggering, and Mean Pressure Shift

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ◽

10.2514/6.2004-4054 ◽

2004 ◽

Author(s):

Gary Flandro ◽

Sean Fischbach ◽

Joseph Majdalani ◽

Jonathan French

Keyword(s):

Rocket Motor ◽

Stability Prediction ◽

Pressure Shift ◽

Prediction Limit ◽

Mean Pressure ◽

Limit Amplitude

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Forced Resonant Shock Waves and Mean Pressure Shift in a Closed Tube

43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ◽

10.2514/6.2007-5806 ◽

2007 ◽

Author(s):

Eric Jacob ◽

Gary Flandro ◽

Daniel Banuti

Keyword(s):

Shock Waves ◽

Pressure Shift ◽

Closed Tube ◽

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Monthly Mean Pressure Reconstructions for Europe (1780-1980) and North America (1858-1980)

Carbon Dioxide Information Analysis Center (CDIAC) Datasets ◽

10.3334/cdiac/cli.ndp025 ◽

1987 ◽

Author(s):

P.D. Jones, ◽

T.M.L. Wigley, ◽

K.F. Briffa,

Keyword(s):

North America ◽

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Performance Optimization of a Straight-Scheme Hybrid Rocket Motor

Физика горения и взрыва ◽

10.15372/fgv20170603 ◽

2017 ◽

Keyword(s):

Performance Optimization ◽

Rocket Motor ◽

Hybrid Rocket ◽

Hybrid Rocket Motor

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Calculation of Pressure in a Solid-Propellant Rocket Motor with the Use of a Real Dependence of the Solid Propellant Burning Rate on Pressure

Физика горения и взрыва ◽

10.15372/fgv20170510 ◽

2017 ◽

Keyword(s):

Burning Rate ◽

Solid Propellant ◽

Rocket Motor ◽

Solid Propellant Rocket ◽

Propellant Rocket

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Lifetime Cycle Testing of Model Nozzles Made of a Carbon--Carbon Composite Material in an Oxygen-Hydrogen Liquid-Propellant Rocket Motor

Прикладная механика и техническая физика ◽

10.15372/pmtf20190111 ◽

2019 ◽

Keyword(s):

Composite Material ◽

Carbon Composite ◽

Rocket Motor ◽

Liquid Propellant ◽

Carbon Composite Material ◽

Propellant Rocket

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CHARACTERIZATION OF NOZZLE EROSION BEHAVIOR UNDER ROCKET MOTOR OPERATING CONDITIONS

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.2011001444 ◽

2010 ◽

Vol 9 (6) ◽

pp. 533-548

Author(s):

Brian Evans ◽

Kenneth K. Kuo ◽

Andrew C. Cortopassi

Keyword(s):

Rocket Motor ◽

Operating Conditions ◽

Erosion Behavior ◽

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EXPERIMENTAL AND NUMERICAL STUDY OF CASTING PROCESS EFFECTS ON SMALL SCALE SOLID ROCKET MOTOR BALLISTIC BEHAVIOR

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.v5.i1-6.160 ◽

2002 ◽

Vol 5 (1-6) ◽

pp. 132-145 ◽

Author(s):

P. Le Breton ◽

D. Ribereau ◽

C. Marraud ◽

P. Lamarque

Keyword(s):

Numerical Study ◽

Casting Process ◽

Rocket Motor ◽

Small Scale ◽

Solid Rocket Motor ◽

Process Effects ◽

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Holographic diagnostics of breakup phenomena of impinging jets for liquid rocket motor applications

International Congress on Applications of Lasers & Electro-Optics ◽

10.2351/1.5058354 ◽

1989 ◽

Author(s):

C. F. Hess ◽

J. D. Trolinger ◽

D. C. Weber ◽

C. P. Wood ◽

G. S. Samuelsen ◽

...

Keyword(s):

Impinging Jets ◽

Rocket Motor ◽

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A study of solid propellant rocket motor command termination by water injection

10.2514/6.1970-640 ◽

1970 ◽

Author(s):

W. GERBER ◽

L. STRAND

Keyword(s):

Solid Propellant ◽

Water Injection ◽

Motor Command ◽

Rocket Motor ◽

Solid Propellant Rocket ◽

Propellant Rocket

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