Solid propellant vehicle to perform probe, re-entry, and orbital research missions may be ground launched or given initial boost by first stage using fin configuration to provide stability; tests to determine effects of fin area, antennas and wiring tunnels on stability at Mach 2.29, 2.96, 3.96, and 4.65 and Re of 3.5×106/ft.
Investigation of static longitudinal and lateral stability characteristics of 0.10-scale model of three-stage configuration of scout research vehicle at Mach numbers of 2.29, 2.96, 3.96, and 4.65
NASA -- Tech Note
1961
27 pages
Report
English
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