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Institution:
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Purdue University-Main Campus
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Subject:
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Description:
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Credit Hours: 3.00. Generalized internal compressible and incompressible flows. Thermochemistry and heat transfer in rocket applications. Advanced topics in solid rocket motor performance and internal ballistics. Liquid rocket engine cycle analysis and turbopump design. Combustion of liquid and solid propellants. Hybrid rockets and thermal-nuclear engines. Typically offered Spring. 3.000 Credit Hours Levels: Graduate, Professional, Undergraduate Schedule Types: Lecture School of Aero and Astro Engr College Aeronautics & Astronautics Department Course Attributes: AE Propulsion, Upper Division
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Credits:
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3.00
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Credit Hours:
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Prerequisites:
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Corequisites:
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Exclusions:
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Level:
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Instructional Type:
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Lecture
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Notes:
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Additional Information:
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Historical Version(s):
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Institution Website:
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Phone Number:
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(765) 494-4600
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Regional Accreditation:
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North Central Association of Colleges and Schools
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Calendar System:
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Semester
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