Angular Momentum and the Aircraft-Store Separation Problem

Abstract

The stability criterion of a missile containing an internal spinning fly wheel is derived and the effect of this fly wheel on the missile's launch disturbance is explained.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1972
Accession Number
AD0749027

Entities

People

  • P. Daniels
  • T. A. Clare

Organizations

  • Naval Surface Warfare Center Dahlgren Division

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Angular Momentum
  • Bearings
  • Center Of Gravity
  • Equations
  • Equations Of Motion
  • External Stores
  • Flight Speeds
  • Gravity
  • High Density
  • Inertia
  • Low Density
  • Moment Of Inertia
  • Momentum
  • Nomenclature

Fields of Study

  • Physics