Development of the NOL Thermal Blast Simulator,

Abstract

A heating method to simulate nuclear weapon thermal radiation effects was developed and combined with an existing airblast simulator the NOL 180-foot Conical Shock Tube. Rapid heating is effected by exposing the target to hot product gases from a burning sheet of solid rocket propellant. The heat transfer process was found to be predominately convective. Fully clamped aluminum plates 9 inches square x 3/32 inch thick were exposed to propellant heating alone, airblast alone, and to propellant heating followed quickly by airblast. Results of these tests have successfully demosntrated the feasibility of simulating thermal readiation-airblast interaction effects on single targets of reasonable scale. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 19, 1972
Accession Number
AD0752023

Entities

People

  • Barry S. Katz
  • Joseph G. Connor Jr.

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Counter WMD
  • Weapons Technologies

DTIC Thesaurus Topics

  • Heat Transfer
  • Nuclear Weapons
  • Propellants
  • Radiation
  • Radiation Effects
  • Rocket Propellants
  • Shock Tubes
  • Simulators
  • Solid Rocket Propellants
  • Thermal Radiation

Fields of Study

  • Physics

Readers

  • Explosive Engineering.
  • Rocket Propulsion.
  • Thermal Physics or Thermal Science.