Pre- and Post-Burning Analysis of Nano-Alluminized Propellants. Comparison of Four Russian Nano-Al Powders

Abstract

Aluminum nano-powders of Russian production were examined and compared with the final goal to evaluate their application in solid rocket propellant formulations. A detailed investigation, concerning a compared characterization of differently sized aluminum powders, by BET (Specific Surface), EM (Electron Microscopy), XRD (X-Ray Diffraction), and XPS (X-ray Photoelectron Spectroscopy), expands the analysis already presented in the first interim report. A detailed investigation concerning a compared characterization of condensed combustion residues of several propellants, based on differently sized aluminum powders, expands the analysis presented in the second interim report. Experimental data concerning the ballistic characterization of several propellants, in terms of steady burning rates and other ballistic effects, expands the analysis already presented in the third interim report. Flame structures and agglomeration phenomena, at and near the burning surface, of several aluminized formulations were analyzed by high-speed, high-resolution, color, digital video recordings. All ballistic studies were performed at SPLab, Milan, Italy using industrial (for comparison) and laboratory composite solid rocket propellants based on ammonium perchlorate as oxidizer and HTPB as binder. The reference formulation was an AP/HTPB/Al composition with respectively 68/17/15 % mass fractions. Results obtained under a wide variety of operating conditions typical of rocket propulsion indicate, for increasing nano-Al mass fraction or decreasing nano-Al size, larger steady burning rates with essentially the same pressure sensitivity. A variety of other effects connected with nano-Al powders appears, depending on the details of the burning formulations. This first year report is focused on uncoated nano-powders of Russian production; the second year report (if continuation is approved) will deal with coated Russian nano-powders and US nanopowders. before any actual use. Witb

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2004
Accession Number
ADA524328

Entities

People

  • Luciano Galfetti
  • Luigi De Luca

Organizations

  • Polytechnic University of Milan

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Chemical Elements
  • Chemical Reaction Properties
  • Chemistry
  • Combustion
  • Composite Propellants
  • Diffraction
  • Electron Microscopy
  • Energetic Materials
  • Isotherms
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Microscopy
  • Rocket Propellants
  • Solid Propellants
  • Solid Rocket Propellants

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics