84-Inch Propellant Cartrides and Grains.

Abstract

This document reports the results obtained from casting a total of 30 84-inch cartridges with UTP-18,803A propellant (90% solids, 21% aluminum, HTPB). Both ballistic and mechanical property data obtained during the production of over 730,000 lbs of propellant is presented. Documentation for propellant production is provided. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 30, 1977
Accession Number
ADA052774

Entities

People

  • Joseph B. Henry
  • Terry V. O'hara
  • Wendell A. Stephen

Organizations

  • United Technologies Corporation

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Combustion
  • Design Criteria
  • Fabrication
  • Failure Mode And Effect Analysis
  • Intercontinental Ballistic Missiles
  • Ions
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Mechanical Properties
  • Mechanics
  • Physical Properties
  • Plastic Explosives
  • Propellant Grains
  • Self Assembly
  • Tensile Strength

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Rocket Propulsion.