Integrated Simulation of Solid Propellant Rockets

نویسندگان

  • William A. Dick
  • Robert A. Fiedler
  • Michael T. Heath
چکیده

This paper presents an overview of research activities at the Center for Simulation of Advanced Rockets (CSAR) at the University of Illinois at Urbana-Champaign. CSAR is one of five university-based research centers funded by the U. S. Department of Energy as part of the Accelerated Strategic Computing Initiative (ASCI). The purpose of ASCI is to advance the state of the art in computational simulation of complex, multicomponent systems and to provide the computational hardware and infrastructure necessary to carry out very large-scale simulations. CSAR is using the solid rocket boosters of the NASA Space Shuttle as the simulation vehicle. Now at the beginning of the fourth year of our ten-year program, the implementation of a fully integrated simulation code is nearly complete and is expected to be finished before the end of 2000. It provides a characterization of various burn scenarios and the onset of potential component failures. Other sub-scale rockets have been simulated to provide verification data for CSAR codes. Refined multiscale component models and advanced system integration concepts based on lessons learned from our current work constitute the key features in the second-generation code targeted for the next few years.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

بررسی پارامترهای موثر بر کهولت پیشرانه‌‌های جامد مرکب بر پایه‌ی HTPB

HTPB based composite Solid propellants are the source of power for the propulsion of rockets and missiles. Since composite solid rocket propellants, used in rockets and missiles is the fastest degrading component of the complete system, shelf life of the system is mainly governed by the life of the propellants. During storage and transportation, the propellant grains are subjected to various co...

متن کامل

Simulations of Slumping Propellant and Flexing Inhibitors in Solid Rocket Motors

* Technical Program Manager † Research Programmer ‡ Visiting Scholar § Research Scientist ¶ Associate Professor of Aeronautical and Astronautical Engineering, University of Illinois at Urbana-Champaign # Postdoctoral Research Associate ** Senior Research Scientist Copyright  2002 by Center for Simulation of Advanced Rockets. Published by the American Institute of Aeronautics and Astronautics, ...

متن کامل

پیشرانه جامد مرکب پرانرژیNEPE(علمی-ترویجی)

Nitrate ester plasticized polyether (NEPE) is a new generation of composite solid propellants which its high energy content in comparing with conventional formulations, has attracted many researchers in the defense departments, all over the world. First of all an introduction and history and importance of NEPE propellants will be discussed and formulation and combination of propellants componen...

متن کامل

Coupled Fluid-structure 3-d Solid Rocket Motor Simulations

* Technical Program Manager † Visiting Scholar ‡ Research Scientist § Associate Professor of Civil and Environmental Engineering, University of Illinois at Urbana Copyright  2001 by Center for Simulation of Advanced Rockets. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Abstract We describe our numerical method for threedimensional simulations of s...

متن کامل

5B.1 Parallel Mesh Adaptation for Highly Evolving Geometries with Application to Solid Propellant Rockets

We describe our parallel 3-D surface and volume mesh modification strategy for large-scale simulation of physical systems with dynamically changing domain boundaries. Key components include an accurate, robust, and efficient surface propagation scheme, frequent mesh smoothing without topology changes, infrequent remeshing at regular intervals or when triggered by declining mesh quality, a novel...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2000