Missile Design Tool (MDT) User's Guide

Abstract

This report provides a User s Guide to the Missile Design Tool (MDT). MDT is a standalone program that can preliminarily estimate several important performance parameters of a solid rocket using aerodynamic and motor information. This report explains the user interface and input at length as well as providing an in-depth explanation of the simulation output and its interpretation.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 2014
Accession Number
ADA597540

Entities

People

  • Andrew Watts
  • John Braswell
  • Mark Underwood
  • Sam Curtis

Organizations

  • United States Army Research, Development and Engineering Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Diameters
  • Differential Equations
  • Engines
  • Equations
  • Flight Paths
  • Geometry
  • Graphical User Interface
  • Nose Cones
  • Payload
  • Propellants
  • Rocket Engines
  • Rockets
  • Simulations
  • Specific Impulse
  • Two Dimensional
  • User Interface

Readers

  • Atmospheric Science/Meteorology
  • Computer Science.
  • Missile Defense Systems.