PSU AERSP 401A - Launch System Selection

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Launch System SelectionSlide 2Slide 3Slide 4Slide 5Launch System Selection(How do we get there from here?)Launch System Selection•System selection process–Define requirements and constraints–Number of spacecraft–Spacecraft mass–Spacecraft dimensions–Mission orbit–Mission timeline–Funding constraintsLaunch System Selection•System selection process–Identify capable systems–Reliability–Performance margin available–Fairing size and shape–Launch Availability–CostLaunch System Selection•System selection process–Analyze capable systems–Maximum accelerations–Vibration frequencies and amplitudes–Acoustic frequencies and amplitudes–Temperature extremes–LV/satellite interface–Kick motor needed?Launch System Selection•References–Wertz, J. R., and Larson, W. J., eds., Space Mission Analysis and Design, 3rd ed. Ch. 18, Microcosm Press, El Segundo, CA,1999.–Isakowitz, S. J., AIAA International Reference Guide to Space Launch Systems, 2nd ed. AIAA Press, Washington DC,


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PSU AERSP 401A - Launch System Selection

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