Pressure correction of ultrasonic regression rate measurements of a hybrid slab motor

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Serin, Nadir ^a   Chiaverini, Martin J ^b,c   Harting, George C ^b   Kuo, Kenneth K ^b  

^a MIDDLE EAST TECHNICAL UNIVERSITY   (Turkey)

^b PENNSYLVANIA STATE UNIVERSITY   (United States)

^c Orbital Technology Corp   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FUELS; PROPULSION; REGRESSION ANALYSIS; ULTRASONIC APPLICATIONS; X RAYS;

CONVENTIONAL THEORY; CORRECTION EQUATION; HYBRID ROCKET MOTORS; MECHANICAL DEFORMATION; PRESSURE CORRECTION; PRESSURE-CORRECTION METHODS; ULTRASONIC PULSE-ECHO METHOD; ULTRASONIC PULSE-ECHO TECHNIQUES;

X RAY RADIOGRAPHY;

EID: 84963805260     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2319     Document Type: Conference Paper

References (8)

1. Kuo, K. K., “Importance and Challenges of Hybrid Rocket Propulsion Beyond Year 2000,” Invited von Karman Lecture in the Proceedings of the 37th Israel Annual Conference on Aerospace Sciences, pp. 1-31, February 26-28, 1997.
2. Sutton, G. P., Rocket Propulsion Elements, 6th Ed., John Wiley & Sons, Inc., 1992.
3. Kuentzmann, P., Demarais, J. C., and Cauty, F., “Mesure de la vitesse de combustion des propergols solides par ultrasons”, La Reserche Aerospatiale, No. 1, pp. 55-79, 1979.
4. Cauty, F., Demarais, J. C., and Erades, C., “Determination of Solid Propellant Burning Rate Sensitivity to the Initial Temperature by the Ultrasonic Method,” Non-Intrusive Combustion Diagnostics, edited by K.K. Kuo and T.P. Parr, Begell House, Inc., New York, 1994, pp. 642-653.
5. Chiaverini, MJ., N. Serin, D.K. Johnson, Y.C. Lu, and K. K. Kuo, “Instantaneous Regression Behavior of HTPB Solid Fuels Burning with GOX in a Simulated Hybrid Rocket Motor,” Challenges in Propellants and Combustion 100 Years After Nobel, Begell House, Inc., New York, pp. 719733, 1997.
6. Chiaverini, M. Kuo, K. K., and Peretz, A., “Regression Rate and Heat Transfer Correlations for HTPB/GOX Combustion in a Hybrid Rocket Engine,” AIAA Paper No. 98-3185, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, OH, July 13-15, 1998.
7. Williams, M., Solid Rocket Technology, edited by Shoir, M., Zaehringer, A. J., John Willey & Sons Inc., 1967.
8. Jana, M. K., Renganathan, K., Venkateswara, R. G., “Effect of Bulk Modulus Variation with Pressure in Propellant Grain Elastic Stress Analysis,” Computers & Structures, Vol. 26, No. 5, pp 761-766, 1987