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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2012
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Article
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Fig 2
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Research Article
Burning Characteristics of Ammonium-Nitrate-Based Composite Propellants with a Hydroxyl-Terminated Polybutadiene/Polytetrahydrofuran Blend Binder
Figure 2
Photograph of propellant quenched at 7 MPa.