Status of Advanced Two-Phase Flow Model Development for SRM Chamber Flow Field and Combustion Modeling

Abstract

This document consists of Briefing charts which provide an overview of the Integrated High Payoff Rocket Propulsion Technology(IHPRPT) Phase III Solid Rocket Motor Modeling Program, presented at the 2004 TFAWS Meeting in Pasadena, CA.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2004
Accession Number
ADA427829

Entities

People

  • Bob Prozan
  • Gary Luke
  • Mark Eagar
  • Michael Sears
  • Scott Felt

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Blast Tubes
  • Boundary Layer
  • Chambers
  • Combustion
  • Combustion Chambers
  • Flow
  • Flow Fields
  • Fluid Mechanics
  • Heat Energy
  • Heat Transfer
  • Materials
  • Materials Science
  • Particle Size
  • Propellants
  • Rocket Engines
  • Thermodynamic Properties
  • Two Phase Flow

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Rocket Propulsion.