Skip to main content
U.S. Department of Energy
Office of Scientific and Technical Information

Solid Rocket Motor Design using a Low-Dimensional Fluid Model

Technical Report ·
DOI:https://doi.org/10.2172/1496883· OSTI ID:1496883
This document is a summary of the mathematical models that are used in the DARPA TRADES project for the solid rocket motor design challenge. It is hoped that this brief description of these models will be of use to those that are working on the project.
Research Organization:
Sandia National Laboratories (SNL-NM), Albuquerque, NM (United States)
Sponsoring Organization:
Defense Advanced Research Projects Agency (DARPA); USDOE National Nuclear Security Administration (NNSA)
DOE Contract Number:
AC04-94AL85000; NA0003525;
OSTI ID:
1496883
Report Number(s):
SAND--2019-1818R; 672713
Country of Publication:
United States
Language:
English

Similar Records

A miniature solid propellant rocket motor
Conference · 1997 · OSTI ID:510333

Model of burning and detonation in rocket motors
Technical Report · 1979 · OSTI ID:5641587

Solid rocket motor internal flow during ignition
Journal Article · 1995 · Journal of Propulsion and Power · OSTI ID:117648