Missile Total and Subsection Weight and Size Estimation Equations

Abstract

This study utilizes regression analysis to develop equations which relate missile overall and subsection weights and geometries, including wings and fins, to variables which are considered to be the input for a new design in the conceptual or preliminary design phase. These variables include packaging requirements such as maximum length, diameter, and weight, as well as performance characteristics such as mission and range. Data for the analysis was collected from a variety of military, industrial, and academic sources. The generic missile is split into three subsections: propulsion, guidance and control, and warhead. Utilizing single and multi-variable regression analysis, weight estimation equations are developed for the total missile, subsections , and wings/fins based on categorizing the missile by mission: air-to-air, air-to- surface, surface-to-air, or surface-to-surface; and by range: short, medium, or long. Measures of fit are developed and displayed with their associated equations to aid in selection of the optimum equation.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1992
Accession Number
ADA256081

Entities

People

  • John B. Nowell Jr.

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Birds
  • Computer Programs
  • Computers
  • Correlation Analysis
  • Data Science
  • Databases
  • Diameters
  • Engineering
  • Guidance
  • Information Science
  • Physical Properties
  • Propulsion Systems
  • Regression Analysis
  • Rocket Propulsion
  • Standards
  • Statistical Analysis
  • United States

Readers

  • Aerodynamics/Aeronautics.
  • Military Science and Technology Research and Modernization.
  • Regression Analysis.