Calculations of the Performance of Explosive Impulse Generators

Abstract

Numerical calculations of the performance of explosive impulse generators were performed. The explosive impulse generators were intended to provide the guidance thrust for a fast response missile guidance system. The objective of the calculations was to provide inforamtion to help determine whether an explosive impulse generator could be designed to produce the required impulse without generating a stress environment within the vehicle body that could cause damage either to the internal electronics or to the remaining undetonated impulse generators. Several 1D finite difference calculations were performed to analyze various buffering or stress attentuation schemes while at the same time estimating the impulse generated by the explosive thruster systems. The 1D analyses show that it may be possible to design a system with the required features but further analysis involving 2D explosive loading/ structural response calculations is required.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1979
Accession Number
ADA079408

Entities

People

  • M. W. Mckay
  • R. N. Schlaug

Tags

Communities of Interest

  • Advanced Electronics
  • Counter IED
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Gaps
  • Contracts
  • Electronics
  • Environment
  • Explosive Charges
  • Explosives
  • Generators
  • Guidance
  • Materials
  • Materials Laboratories
  • Rocket Engines
  • Shock Waves
  • Stagnation Pressure
  • Stress Waves
  • Structural Response
  • Thrusters
  • Waves

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster