Heat Flux and Infrared Spectral Measurements of Burning SRM Propellant (Postprint)

On 23 August 2005 the Air Force Research Laboratory (AFRL) Propulsion Directorate at Edwards AFB conducted an open air burn of over 2000 kg of Titan IV solid rocket motor propellant. Multiple remote sensors were deployed to measure the heat flux and spectral emissions during the burn. The heat flux...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Venner, Marty, Parker, James, McKeon, William
Format: Report
Sprache:eng
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