The objective of the materiel test procedure is to describe the engineering tests required to obtain data on missile aerodynamics during actual flight conditions. Flight characteristics such as force and moment coefficients, heating effects and aeroelastic effects and aeroelastic effects are to be determined. Preliminary missile parameters derived from analytical techniques and wind tunnel testing are verified and updated. Missile performance characteristics and flight safety boundaries are to be established. (Author)
Investigation of Missile System Aerodynamics
1970
16 pages
Report
No indication
English
NTIS | 1998
SLUB | 1988
|NTIS | 1979
NTIS | 1990