Accession Number:

ADA034201

Title:

A Study of Various Slender and Non-Slender Fin-Body Combinations of Missile Configurations.

Descriptive Note:

Technical rept.,

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL ALA AEROBALLISTICS DIRECTORATE

Personal Author(s):

Report Date:

1976-11-12

Pagination or Media Count:

189.0

Abstract:

The aerodynamic loading on a number of rocket body-control surface combinations has been calculated using methods developed at the University of Tennessee Space Institute over the past five years. Variations in control surface planform, roll angle, control surface deflection or incorporation of elevons, are included. Compressibility is accounted for. Details of the digital computer program are included.

Subject Categories:

  • Aerodynamics
  • Rockets

Distribution Statement:

APPROVED FOR PUBLIC RELEASE