Solid Body Equations to Calculate the Trajectory of Ramjet

Abstract

Six-degree-of-freedom trajectory equations for a ramjet propelled, gun launched projectile are formulated. An outline for FORTRAN computer program flow charts also appear in the report. Special emphasis is given to the effect of wind on trajectory errors.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1982
Accession Number
ADA118241

Entities

People

  • Kenji Imai

Tags

DTIC Thesaurus Topics

  • Air Temperature
  • Ascent Trajectories
  • Bodies
  • Center Of Gravity
  • Computer Programs
  • Computers
  • Coordinate Systems
  • Drag
  • Equations
  • Exterior Ballistics
  • Flow
  • Gravity
  • Launching
  • Procedures (Computers)
  • Solid Bodies
  • Trajectories
  • Trim Angle

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Missile Defense Systems.