Enhancing Composite Solid Propellant Burning Rates with Potassium Doped Ammonium Perchlorate—Part 2-Reference-Cited by-同舟云学术

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Enhancing Composite Solid Propellant Burning Rates with Potassium Doped Ammonium Perchlorate—Part 2

Published:2014-07 Issue:4 Volume:30 Page:876-882
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Ishitha Kumar¹,Ramakrishna P. A.¹

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600 036, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35236

Reference17 articles.

1. KubotaN., Propellants and Explosives, Wiley, Weinheim, Germany, 2002, p. 87.

2. MukundaH. S., Understanding Aerospace Chemical Propulsion, Interline, India, 2004, p. 275.

3. WilliamsF. A.BarrereM.HuangN. C., Fundamental Aspects of Solid Propellant Rockets, Technivision, Slough, England, 1964, pp. 531–533.

4. Dependence of density and burning rate of composite solid propellant on mixer size

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1. An alternative approach to improve burning rate characteristics and processing parameters of composite propellant;Combustion and Flame;2019-11

2. Use of X‐Ray Computed Tomography for Validation of Random Packs of Composite Solid Propellants;Propellants, Explosives, Pyrotechnics;2019-04-17

3. Ferrocene grafted hydroxyl terminated polybutadiene: A binder for propellant with improved burn rate;Polymer;2019-02

4. Porous Cr2O3 bead with a 3D continuous pore architecture: synthesis and its catalytic performance for decomposition of ammonium perchlorate;New Journal of Chemistry;2019

5. Effect of Curing Agent on the Plateau Burning Mechanism of Solid Propellant Sandwiches;Journal of Propulsion and Power;2018-11

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