RETRACTED: Effect of nozzle thermal environment on the ablation rate of the throat inserts of solid rocket motors
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Abstract
This article has been retracted at the request of the editor due to incorrect format. Therefore, it has been corrected and replaced.
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Source: openaire · Quality: needs review · Source record ↗
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Research context
OpenAlex topics: Rocket and propulsion systems research · Energetic Materials and Combustion · Field-Flow Fractionation Techniques
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References (20)
Show source-provided references
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