Internal flow analysis of large L/D solid rocket motors

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Laubacher, Brian A ^a  

^a Thiokol Propulsion   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTICS; COMPUTATIONAL FLUID DYNAMICS; FLOW FIELDS; ROCKET ENGINES; SPACE SHUTTLES; SPACECRAFT PROPULSION;

COMPUTATIONAL FLUID DYNAMICS ANALYSIS; GEOMETRICAL CHARACTERISTICS; INTERNAL BALLISTIC; LENGTH TO DIAMETER RATIO; PREDICTED PERFORMANCE; PROPELLANT GRAIN; REUSABLE SOLID ROCKET MOTORS; SOLID ROCKET MOTORS;

ROCKETS;

EID: 34249283926     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. "The Solid Propellant Rocket Motor Performance Prediction Computer Program (SPP)," Software and Engineering Associates, Inc., Carson City Nevada.
2. "A User's Guide for Computer Program No. SCB02, An Internal Ballistics Program for Segmented Solid Propellant Rocket Motors," Thiokol Propulsion, 1982
3. Clayton, C. D., "Flow Fields in Solid Rocket Motors With Tapered Bores," AIAA Paper 96-2643.
4. Gruet, L., "QM-7 and QM-8. Transient Axial Pressure Calculated From Strain Gauge Data," TWR-63695, Thiokol Corporation, 30. March 1992.
5. Salita, M., "Verification of Spatial and Temporal Pressure Distributions in Segmented Solid Rocket Motors," AIAA Paper 89-0298.
6. Loh, H.T. and Golafshani, M., "Computation of Viscous Chemically Reacting Flows in Hybrid Rocket Motors Using an Upwind LU-SSOR Scheme," AIAA paper 90-1570.
7. Loh, H.T., Smith-Kent, R., Perkins, F., and Chwalowski, P., 1996, "Evaluation of Aft Skirt Length Effects on Rocket Motor Base Heat Using Computational Fluid Dynamics," AIAA paper 96- 2645.
8. Loh, H. T., Chwalowski, P., "One and Two-Phase Converging Diverging Nozzle Flow Study," AIAA Paper 95-0084.
9. Beddini, R. A., "Injection-Induced Flows in Porous- Walled Ducts," AIAA Journal, Vol. 24. No, 11, Nov. 1986, pp. 1766-1773.
10. King, M. K., "Consideration of Two-Dimensional Flow Effects on Nozzleless Rocket Performance," AIAA paper 84-1313.
11. Traineau, J-C., Hervat, P., Kuentzmann, P., "Cold- Flow Simulation of a Two-Dimensional Nozzleless Solid Rocket Motor," AIAA Paper 86-1447.
12. Culick, F. E. C., "Rotational Axisymmetric Mean flow and Damping of Acoustic Waves in a Solid Propellant Rocket," AIAA Journal, Vol. 4, No. 8, 1966, pp. 1462-1464.