Accession Number : AD0290930

Title :   ANALYSIS OF MISSILE LAUNCHERS. PART 02 CURVATURE IN RIGID RAIL LAUNCHERS MODELS

Corporate Author : ILLINOIS UNIV URBANA

Personal Author(s) : PENROD,D. ; STERN,M.

Report Date : SEP 1962

Pagination or Media Count : 1

Abstract : An analysis of the single degree of freedom model of rigid rail launchers including the effects of arbitrary rail curvature and tipoff is presented. The equations are put in a form suitable for solution by analog computer and some illustrative numerical results are presented. (Author)

Descriptors :   *GUIDED MISSILE LAUNCHERS, *ROCKET LAUNCHERS, ANALOG COMPUTERS, CURVED PROFILES, EQUATIONS, MATHEMATICAL ANALYSIS, MATHEMATICAL MODELS, MOTION

Distribution Statement : APPROVED FOR PUBLIC RELEASE