A wind tunnel test was conducted using 0.05-scale models to study the separation characteristics of the SUU-51/B from the F-4C aircraft. The separation trajectories were initiated from the left-wing inboard pylon station utilizing the Triple Ejection Rack and from the centerline pylon utilizing the Multiple Ejection Rack. The flight conditions simulated were Mach numbers from 0.66 to 0.90 at an altitude of 5000 ft. Parent aircraft dive angles of 0, 30, and 45 deg were simulated. (Author)
Separation Characteristics of the SUU-51/B from the F-4C Aircraft
1971
66 pages
Report
Keine Angabe
Englisch
Bombs , Detonations, Explosion Effects, & Ballistics , Cluster warheads , Free flight trajectories , Jet fighters , External stores , Wind tunnel models , Model tests , Angle of attack , Subsonic characteristics , Ejection , Exterior ballistics , Bomb trajectories , Separation , Trajectories , F-4 aircraft , F-4c aircraft , Suu-51/b dispensers
Prediction of JDAM Separation Characteristics from the F/A-18C Aircraft
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