Solid Rocket Motor Design using a Low-Dimensional Fluid Model
- Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
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
Model of burning and detonation in rocket motors
Solid rocket motor internal flow during ignition
Conference
·
Fri Aug 01 00:00:00 EDT 1997
·
OSTI ID:510333
Model of burning and detonation in rocket motors
Technical Report
·
Mon Dec 31 23:00:00 EST 1979
·
OSTI ID:5641587
Solid rocket motor internal flow during ignition
Journal Article
·
Mon May 01 00:00:00 EDT 1995
· Journal of Propulsion and Power
·
OSTI ID:117648