ANALYSIS OF MISSILE LAUNCHERS. PART 02 CURVATURE IN RIGID RAIL LAUNCHERS MODELS
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1962
- Accession Number
- AD0290930
Entities
People
- D. Penrod
- M. Stern
Organizations
- University of Illinois Urbana–Champaign