This memorandum establishes accuracy requirements for the various items measured during re-entry for the determination of nose cone aero-thermodynamic parameters. The results are applicable, unless otherwise specified, for a variety of nose cone configurations and re-entry trajectories typical of 7-1, 7-3 and 7-0 missiles. (Author)
Accuracy of Re-Entry Flight Test Data Needed to Determine Re-Entry AERO-Thermodynamic Parameters
1954
19 pages
Report
Keine Angabe
Englisch
Angle of attack , Nose cones , Drag , Surface temperature , Heat transfer , Conical bodies , Pressure , Atmosphere entry , Aerodynamic heating , Missile Technology , Reentry vehicles , Titan , Laminar boundary layer , Mathematical analysis , Surface to surface missiles , Telemetering data , Physics , Accuracy , Thermal stresses
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