Evaluation of nozzle erosion characteristics utilizing a rocket motor simulator

Brian Evans, Peter J. Ferrara, Jeffrey D. Moore, Eric Boyd, Nicholas A. Favorito, Kenneth K. Kuo

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Scopus citations

Abstract

This research addresses scientific understanding and methods for mitigation of rocket nozzle erosion by solid-propellant combustion products in order to substantially increase the operating pressures of future missiles. Several processes can affect the nozzle erosion rate at high-pressure and high-temperature conditions. To characterize the nozzle erosion processes at both traditional operating pressures and at substantially increased pressure levels, two separate test facilities have been planned for operation at chamber pressures up to 8000 psi (55.2 MPa). The focus of this paper is the design and development of one of these test rigs, the rocket motor simulator (RMS). The RMS is a gaseous reactant combustor used to simulate propellent product species generated from a selected non-metallized Propellent S. Utilizing a bi-directional counter-flow vortex combustion chamber, the gaseous reactants are mixed and combusted producing a gaseous mixture with temperature and concentrations of selected oxidizing species similar to those of Propellent S. The ability to control the product species concentrations through gaseous reactant flow rates allows the evaluation of the effect individual chemical species have on the nozzle erosion process. As a means of mitigating erosion of the nozzle throat, a nozzle boundary-layer control system is also adopted in the nozzle assembly design to evaluate the methodology of boundary-layer cooling as a means of controlling erosion rates. Instantaneous erosion rates will be measured using a real-time X-ray radiography system in combination with the X-ray translucent nozzle assembly.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages8850-8862
Number of pages13
ISBN (Print)1563478188, 9781563478185
DOIs
StatePublished - 2006
EventAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference - Sacramento, CA, United States
Duration: Jul 9 2006Jul 12 2006

Publication series

NameCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
Volume11

Other

OtherAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
CountryUnited States
CitySacramento, CA
Period7/9/067/12/06

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Energy(all)
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

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