Recent progress in SRM ignition transient modeling

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Wang, J C T ^a   Landsbaum, E M ^a   Cozart, A B ^a   Frolik, S A ^a   Lee, I ^a  

^a AEROSPACE CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; PROPULSION; WELL TESTING;

CFD APPROACHES; CFD SIMULATIONS; CHAMBER PRESSURE; EROSIVE BURNING; IGNITION TRANSIENT; PROPELLANT SURFACES; RECENT PROGRESS; STATIC FIRING;

RELUCTANCE MOTORS;

EID: 85086492350     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5115     Document Type: Conference Paper

References (17)

1. Wang, J. C. T., "Modern SRM Ignition Transient Modeling (Part 5): Prospective Developments in CFD Simulation, " AIAA paper 2001-3447, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 8-11 July 2001, Salt Lake City, Utah.
2. Landsbaum, E. M., "Erosive Burning Revisited, " AIAA paper, 2003-4805, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 20-23, 2003, Huntsville, AL.
3. Salita, M., "Rocket Propellant Ignition: A Workshop Report, " Proceedings of the 22nd JANNAF Combustion Meeting, Vol. I 1985, pp 65-86.
4. Heath, M., "Whole-system Simulation of Solid Rockets Is Goal of ASCI Center at Illinois, " SIAM News Volume 31, No. 4, May 1998.
5. Luke, G. D., Eagar, M. A., and Dwyer, H. A., "Ignition Transient Model for Large Aspect Ratio Solid Rocket Motor, " AIAA paper 96-3273, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, 1996 Lake Buena, FL.
6. Le Helley, P., "3D Turbulent Navier-Stokes Simulations of Ignition Transients in Solid Rocket Motors, " AIAA Paper 98-3843, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, July 13-15, 1998.
7. Alvilli, J. Buckmaster, J., Jackson, T. L., and Short, M., "Ignition-transient Modeling for Solid Propellant Rocket Motor, " AIAA paper 2000-3567, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 16-18, 2000, Huntsville, AL.
8. Peretz, A., Kuo, K. K., Caveny, L. H., and Summerfield, M. "Starting Transient of Solid-Propellant Rocket Motors with High Internal Gas Velocities, " AIAA Journal, Vol. 11, No. 12, 1973, pp 1719-1727.
9. Churchill, R. V., "Operational Mathematics, " 3rd Ed., Section 47, McGraw-Hill, 1958, p150.
10. Johnston, W. A. "Solid Rocket Motor Internal Flow During Ignition, " AIAA paper 91-1655, also AIAA Journal of Propulsion and Power, Vol. 11, No. 3, 1995, pp 489-496.
11. Keith, F., Principles of Heat Transfer, 2nd Edition, International Textbook Co., 1965.
12. Ton, V. T. Wang, J. C. T., and Widhopf, G. F., "Segmented Solid Rocket Motor Internal Flow Simulations, " AIAA Paper 90-0683, 1990.
13. Wang, J. C. T., and Taylor, S., "Large Scale Navier-Stokes Multi-Body Launch Vehicle Flowfield Simulations, " Proceedings, 20th Congress of International Council.
14. Wang, J. C. T. and Widhopf, G. F., "A High-Resolution TVD Finite Volume Scheme for the Euler Equations in Conservation Law Form, " AIAA Paper 87-0538; also, Journal of Computational Physics, Vol. 84, No. 1, 1989, pp 145-173.
15. "Solid Rocket Motor Internal Insulation, " NASA SP-8903, 1976.
16. Wang, J. C. T., Yang. S. H., Than, P. T. and Ndefo, E. D., "Coupled Transient Flowfield and Propellant Deformation Analysis for the Titan IV 7-Segment Solid Rocket Motor, " AIAA Paper 94-3285, 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, June 27-29, 1994, Indianapolis, IN.
17. Saderholm, C. A., "A Characterization of Erosive Burning for Composite H-Series Propellants, " AIAA Solid Propellant Rocket Conf., Palo Alto, CA, Jan. 29, 1964.