THEORY OF PROPULSION 4' Nozzles - PowerPoint PPT Presentation

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THEORY OF PROPULSION 4' Nozzles

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USAF AEDC Rocket Test Cell ... 5.16 was designed for h=30.5km but launch takes place at sea level (p=101.3kPa) ... Courtesy NASA. 2-D Variable Area Nozzle ... – PowerPoint PPT presentation

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