Tests conducted on model designed for orbital, probe and re-entry missions, through angle of attack range from -8 to 8° at average test of 4.0×106 Re/ft; variation of peak negative pressures associated with corners at nose and transition flare may cause critical local loading condition to occur at Mach close to 0. 90; effects of adding protuberances presented.
Aerodynamic loading characteristics at Mach numbers from 0.80 to 1.20 of 1/10-scale three-stage scout model
NASA -- Tech Notes
1961
64 pages
Report
English
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