Constitutive response and damage in solid propellants

N. Aravas, F. Xu, P. Sofronis, A. Namazifard, R. Fiedler

Research output: Contribution to conferencePaper

2 Citations (Scopus)

Abstract

Solid propellants are composite materials with complex microstructure. In a generic form, the material consists of polymeric binder, ceramic oxidizer, and fuel particles (e.g. aluminum). Damage induced by severe stress and extreme temperatures is manifested in particle cracking, decohesion along particle/polymer interfaces, and void opening. In this work, the effect of damage due to particle dewetting on the material macroscopic response is investigated by accounting for large deformations. First, issues pertaining to the constitutive behavior of the individual components in the absence of damage are reviewed. Next, with the use of rigorous composite homogenization theory, a macroscopic constitutive law is devised that accounts for continuous void nucleation and growth upon straining. The standard relaxation and uniaxial tension tests are used to calibrate the model parameters. The model is implemented in our Center's finite element code Rocsolid to study damage evolution in the propellant grain of the Titan IV SRMU PQM-1 rocket motor.

Original languageEnglish
Publication statusPublished - Dec 1 2005
Externally publishedYes
Event41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit - Tucson, AZ, United States
Duration: Jul 10 2005Jul 13 2005

Other

Other41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
CountryUnited States
CityTucson, AZ
Period7/10/057/13/05

Fingerprint

Solid propellants
Rocket engines
Composite materials
Propellants
Binders
Nucleation
Aluminum
Microstructure
Polymers
Temperature

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

Cite this

Aravas, N., Xu, F., Sofronis, P., Namazifard, A., & Fiedler, R. (2005). Constitutive response and damage in solid propellants. Paper presented at 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United States.

Constitutive response and damage in solid propellants. / Aravas, N.; Xu, F.; Sofronis, P.; Namazifard, A.; Fiedler, R.

2005. Paper presented at 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United States.

Research output: Contribution to conferencePaper

Aravas, N, Xu, F, Sofronis, P, Namazifard, A & Fiedler, R 2005, 'Constitutive response and damage in solid propellants', Paper presented at 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United States, 7/10/05 - 7/13/05.
Aravas N, Xu F, Sofronis P, Namazifard A, Fiedler R. Constitutive response and damage in solid propellants. 2005. Paper presented at 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United States.
Aravas, N. ; Xu, F. ; Sofronis, P. ; Namazifard, A. ; Fiedler, R. / Constitutive response and damage in solid propellants. Paper presented at 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United States.
@conference{326c54a24773486094acabe4a7d7ca1a,
title = "Constitutive response and damage in solid propellants",
abstract = "Solid propellants are composite materials with complex microstructure. In a generic form, the material consists of polymeric binder, ceramic oxidizer, and fuel particles (e.g. aluminum). Damage induced by severe stress and extreme temperatures is manifested in particle cracking, decohesion along particle/polymer interfaces, and void opening. In this work, the effect of damage due to particle dewetting on the material macroscopic response is investigated by accounting for large deformations. First, issues pertaining to the constitutive behavior of the individual components in the absence of damage are reviewed. Next, with the use of rigorous composite homogenization theory, a macroscopic constitutive law is devised that accounts for continuous void nucleation and growth upon straining. The standard relaxation and uniaxial tension tests are used to calibrate the model parameters. The model is implemented in our Center's finite element code Rocsolid to study damage evolution in the propellant grain of the Titan IV SRMU PQM-1 rocket motor.",
author = "N. Aravas and F. Xu and P. Sofronis and A. Namazifard and R. Fiedler",
year = "2005",
month = "12",
day = "1",
language = "English",
note = "41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; Conference date: 10-07-2005 Through 13-07-2005",

}

TY - CONF

T1 - Constitutive response and damage in solid propellants

AU - Aravas, N.

AU - Xu, F.

AU - Sofronis, P.

AU - Namazifard, A.

AU - Fiedler, R.

PY - 2005/12/1

Y1 - 2005/12/1

N2 - Solid propellants are composite materials with complex microstructure. In a generic form, the material consists of polymeric binder, ceramic oxidizer, and fuel particles (e.g. aluminum). Damage induced by severe stress and extreme temperatures is manifested in particle cracking, decohesion along particle/polymer interfaces, and void opening. In this work, the effect of damage due to particle dewetting on the material macroscopic response is investigated by accounting for large deformations. First, issues pertaining to the constitutive behavior of the individual components in the absence of damage are reviewed. Next, with the use of rigorous composite homogenization theory, a macroscopic constitutive law is devised that accounts for continuous void nucleation and growth upon straining. The standard relaxation and uniaxial tension tests are used to calibrate the model parameters. The model is implemented in our Center's finite element code Rocsolid to study damage evolution in the propellant grain of the Titan IV SRMU PQM-1 rocket motor.

AB - Solid propellants are composite materials with complex microstructure. In a generic form, the material consists of polymeric binder, ceramic oxidizer, and fuel particles (e.g. aluminum). Damage induced by severe stress and extreme temperatures is manifested in particle cracking, decohesion along particle/polymer interfaces, and void opening. In this work, the effect of damage due to particle dewetting on the material macroscopic response is investigated by accounting for large deformations. First, issues pertaining to the constitutive behavior of the individual components in the absence of damage are reviewed. Next, with the use of rigorous composite homogenization theory, a macroscopic constitutive law is devised that accounts for continuous void nucleation and growth upon straining. The standard relaxation and uniaxial tension tests are used to calibrate the model parameters. The model is implemented in our Center's finite element code Rocsolid to study damage evolution in the propellant grain of the Titan IV SRMU PQM-1 rocket motor.

UR - http://www.scopus.com/inward/record.url?scp=77957856690&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=77957856690&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:77957856690

ER -