Four-stage solid propellant missile may be used as 3-stage missile by omitting first stage and adding fins to second stage flare; study made to determine effect of fin area and second stage flare angle on static longitudinal stability; results obtained.
Investigation of static longitudinal stability characteristics of 0. 067-scale of model of four-stage configuration of scout research vehicle at mach numbers of 2.29, 2.96, 3.96, and 4.65
NASA -- Tech Note
1960
25 pages
Report
English
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