Depressurization Extinguishment of Composite Solid Propellants: Flame Structure, Surface Characteristics, and Restart Capability

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• †Deutsche Forschungs- und VerssuchsaKllt für Luft-Raumfahrt e.V. (DFVLR), Institut für Chemische Raketenantriebe, 3041 Trauen ü. Soltau/Hann., W. Germany.
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