Transonic Wind-Tunnel Tests of A 1/15-Scale Model of the TALOS 6cl Missile,

Abstract

Tests of a 1/15-scale model of the TALOS 6cl missile were performed in the TMB 7- by 10-Foot Transonic Wind Tunnel for a Mach number range of 0.7 to 1.17, at angles of attack of -4 to 10, and roll angles of 0 and -45. The investigation included evaluation of the effects of ram-air bleed at the base of the second stage and the longitudinal stability and control effectiveness of the missile. The data are presented without analysis. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1961
Accession Number
ADA062289

Entities

People

  • Michael E. Mcdonald

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Dynamic Pressure
  • Free Stream
  • Intellectual Property
  • Mach Number
  • Model Basins
  • Models
  • Network Protocols
  • Physics Laboratories
  • Scale Models
  • Ship Model Basins
  • Static Pressure
  • Strain Gages
  • Test And Evaluation
  • Transonic Wind Tunnels
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Dynamics.
  • Missile Defense Systems.