Aerodynamic Performance and Stability Coefficients for the XSM-65A Missile.

Abstract

The report documents the results of a study in which the aerodynamic stability and performance coefficients of the XSM-65A missile were determined for the range of flight conditions encountered during the powered flight phase of the missile trajectory. The study was undertaken to provide criteria for missile autopilot and roll control system design and data for use in trajectory performance computations. (AUTHOR)

Document Details

Document Type
Technical Report
Publication Date
Apr 04, 1956
Accession Number
AD0842595

Entities

People

  • R. G. Norell

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Stability
  • Air Traffic Control Systems
  • Automatic Pilots
  • Coefficients
  • Computations
  • Control Systems
  • Entry Control Systems
  • Trajectories

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation
  • Control Systems Engineering.