The report presents the results of a study of the balloting behavior of a rocket on a straight rail launcher. Numerical computations were made for two angles of elevation and are presented in graphical form. (Author)
Data Acquisition and Reduction. Phase Vi, Part I: Balloting Phenomena in Rocket-Launcher Firings
1964
2 pages
Report
No indication
English
ROCKETS , ROCKET LAUNCHERS , VIBRATION , NUMERICAL ANALYSIS , FORCE (MECHANICS) , DATA , MOTION , DESIGN , EQUATIONS , REDUCTION , BALLOTING PHENOMENA