Burning Rate of Solid Propellant Ingredients, Part 2: Determination of Burning Rate Temperature Sensitivity

A. I. Atwood; T. L. Boggs; P. O. Curran; T. P. Parr; D. M. Hanson-Parr; C. F. Price; J. Wiknich

doi:10.2514/2.5523

Burning Rate of Solid Propellant Ingredients, Part 2: Determination of Burning Rate Temperature Sensitivity

Journal of Propulsion and Power ◽

10.2514/2.5523 ◽

1999 ◽

Vol 15 (6) ◽

pp. 748-752 ◽

Cited By ~ 40

Author(s):

A. I. Atwood ◽

T. L. Boggs ◽

P. O. Curran ◽

T. P. Parr ◽

D. M. Hanson-Parr ◽

...

Keyword(s):

Burning Rate ◽

Temperature Sensitivity ◽

Solid Propellant

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Wavelet analysis in ultrasonic determination of solid propellant burning rate

2010 11th International Conference and Seminar on Micro/Nanotechnologies and Electron Devices ◽

10.1109/edm.2010.5568795 ◽

2010 ◽

Author(s):

Valery G. Efimov ◽

Julia N. Lozhkova

Keyword(s):

Wavelet Analysis ◽

Burning Rate ◽

Solid Propellant ◽

Ultrasonic Determination

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Temperature sensitivity coefficients of solid propellant burning rate

Acta Astronautica ◽

10.1016/0094-5765(86)90044-5 ◽

1986 ◽

Vol 13 (3) ◽

pp. 127-130 ◽

Cited By ~ 9

Author(s):

Michael T. Gaunce ◽

John R. Osborn

Keyword(s):

Burning Rate ◽

Temperature Sensitivity ◽

Solid Propellant ◽

Sensitivity Coefficients

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Determination of the coefficient of the temperature sensitivity of the burning rate for condensed systems from the heat conduction equation

High Temperature ◽

10.1134/s0018151x1301015x ◽

2013 ◽

Vol 51 (1) ◽

pp. 106-110 ◽

Cited By ~ 1

Author(s):

O. F. Shlenskii ◽

N. B. Shcherbak ◽

N. N. Lyasnikova

Keyword(s):

Heat Conduction ◽

Burning Rate ◽

Temperature Sensitivity ◽

Heat Conduction Equation ◽

Conduction Equation ◽

Condensed Systems

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Temperature sensitivity of solid propellant burning rate.

AIAA Journal ◽

10.2514/3.4021 ◽

1967 ◽

Vol 5 (3) ◽

pp. 586-587 ◽

Cited By ~ 22

Author(s):

ROBERT L. GLICK

Keyword(s):

Burning Rate ◽

Temperature Sensitivity ◽

Solid Propellant

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DETERMINATION OF SOLID PROPELLANT BURNING RATE SENSITIVITY TO THE INITIAL TEMPERATURE BY THE ULTRASONIC METHOD

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.v3.i1-6.620 ◽

1994 ◽

Vol 3 (1-6) ◽

pp. 642-653

Author(s):

J. CI. Demarais ◽

Franck Cauty ◽

Ch. Erades

Keyword(s):

Burning Rate ◽

Solid Propellant ◽

Initial Temperature ◽

Ultrasonic Method ◽

Rate Sensitivity

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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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TEMPERATURE SENSITIVITY MEASUREMENTS AND REGRESSION BEHAVIOR OF A FAMILY OF BORON-BASED VERY HIGH BURNING RATE PROPELLANTS

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.v2.i1-6.270 ◽

1991 ◽

Vol 2 (1-6) ◽

pp. 438-452

Author(s):

R. M. Salizzoni ◽

W. H. Hsieh ◽

Kenneth K. Kuo

Keyword(s):

Burning Rate ◽

Temperature Sensitivity ◽

Very High

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Burning rate temperature sensitivity of HMX propellants

10.2514/6.1986-1593 ◽

1986 ◽

Author(s):

N. KUBOTA ◽

H. OKUHARA

Keyword(s):

Burning Rate ◽

Temperature Sensitivity

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On the Effectiveness of Using the Real Law of Solid Propellant Burning Rate As a Function of Solid Rocket Motor Pressure

Combustion Explosion and Shock Waves ◽

10.1134/s0010508220020082 ◽

2020 ◽

Vol 56 (2) ◽

pp. 172-180

Author(s):

A. M. Lipanov ◽

L. N. Kolesnikova ◽

A. Yu. Leshchev

Keyword(s):

Burning Rate ◽

Solid Propellant ◽

Rocket Motor ◽

Solid Rocket Motor ◽

The Real ◽

Solid Rocket

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Relative Dispersion of Catalytic Nanoparticle Additives and AP Particles in Composite Solid Propellant and the Effect on Burning Rate

49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ◽

10.2514/6.2011-418 ◽

2011 ◽

Cited By ~ 9

Author(s):

Kevin Kreitz ◽

Eric Petersen ◽

David Reid ◽

Sudipta Seal

Keyword(s):

Burning Rate ◽

Solid Propellant ◽

Relative Dispersion ◽

Composite Solid Propellant ◽

Composite Solid ◽

Nanoparticle Additives

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