A FORTRAN PROGRAM TO CALCULATE A SURFACETO-AIR MISSILE TRAJECTORY.
Abstract
This program computes a trajectory from launch or any point thereafter to any other time or to impact. Point masses and a nonrotating oblate spheroid earth are assumed. The program is written in FORTRAN IV and is used on the IBM 7040 computer. It will accommodate a one, two, or three stage vehicle. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1964
- Accession Number
- AD0602220
Entities
People
- C. F. Ostner
- H. S. Dupree
- W. B. Warren