Impulse generated by a shock tube in a vacuum

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Takashima, Yasuhiro ^a   Kasahara, Jiro ^a   Shepherd, Joseph E ^b   Funaki, Ikko ^c,d  

^a UNIVERSITY OF TSUKUBA   (Japan)

^b Safety and Mission Assurance Manager Space Systems Loral   (United States)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^d Department of Science   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AMBIENT PRESSURES; ATMOSPHERIC ENVIRONMENT; BALLISTIC PENDULUM; DEPRESSURIZATIONS; DETONATION TUBES; DIMENSIONAL ANALYSIS; EFFECT OF VIBRATION; EXHAUST VELOCITY; GAS FILLING; GAS TYPE; IN-VACUUM; METHOD OF CHARACTERISTICS; PARTIAL FILLING; RAREFIED GAS; SHOCK-TUBE DRIVERS; SINGLE PARAMETER; SPECIFIC IMPULSE; SQUARE ROOTS; TIME-SCALES; TRANSLATIONAL ENERGY; TUBE LENGTH; VACUUM CHAMBERS;

AEROSPACE ENGINEERING; ARGON; DETONATION; EXHAUST GASES; HELIUM; NITROGEN; SHOCK TUBES; SULFUR; SULFUR HEXAFLUORIDE; VACUUM;

TUBES (COMPONENTS);

EID: 78149436459     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

1. Roy, G. D., Frolov, S. M., Borisov, A. A., and Netzer, D. W., "Pulse detonation propulsion: challenges, current status, and future perspective," Prog. Energy Combust. Sci., Vol. 30, 2004, pp. 545-672.
2. Zhdan, S. A., Mitrofanov, V. V., and Sychev, A. I., "Reactive Impulse from the Explosion of a Gas Mixture in a Semi-infinite Space," Combustion, Explosion and Shock Waves, Vol. 30, No. 5, 1994, pp. 657-663.
3. Zitoun, R. and Desbordes, D., "Prospective Performances of Pulsed Detonations," Comb. Sci. Tech., Vol. 144, No. 1, 1999, pp. 93-114.
4. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 8-11, 2001, Salt Lake City, UT, AIAA, 2001-3815.
5. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July, 2002, Indianapolis.
6. Cooper, M. A., Impulse Generation by Detonation Tubes, Ph.D. thesis, California Institute of Technology, Pasadena, California, May 2004.
7. Cooper, M., Shepherd, J. E., and Schauer, F., "Impulse correlation for partially-filled tubes," Journal of Propulsion and Power, Vol. 20, No. 5, 2004, pp. 947-950, (Preprint - see journal for final version).
8. Li, C. and Kailasanath, K., "Performance Analysis of Pulse Detonation Engines with Partial Fuel Filling," Journal of Propulsion and Power, Vol. 19 (5), 2003, pp. 908-916.
9. Kasahara, J., Arai, T., and Matsuo, A., "Experimental Analysis of Pulse Detonation Engine Performance by Pressure and Momentum Measurements," AIAA 03-0893.
10. Endo, T., Kasahara, J., Matsuo, A., Inaba, K., Sato, S., and Fujiwara, T., "Pressure History at the Thrust Wall of a Simplified Pulse Detonation Engine," AIAA Journal, Vol. 42, No. 9, September, 2004, pp. 1921-1930.
11. Kasahara, J., Tanahashi, Y., Hirano, M., Numata, T., Matsuo, A., and Endo, T., "Experimental Investigation of Momentum and Heat Transfer in Pulse Detonation Engine," AIAA 04-0869.
12. Sato, S., Matsuo, A., Endo, T., and Kasahara, J., "Numerical Studies on Specific Impulse of Partially Filled Pulse Detonation Rocket Engines," Journal of Propulsion and Power, Vol. 22, No. 1, 2006, pp. 64-69.
13. Endo, T., Yatsufusa, T., Taki, S., Matsuo, A., Inaba, K., and Kasahara, J., "Homogeneous-Dilution Model of Partially Fueled Simplified Pulse Detonation Engines," Journal of Propulsion and Power, Vol. 23, No. 5, September-October, 2007, pp. 1033-1041.
14. th International Colloquium on the Dynamics of Explosion and Reactive Systems, Paper 65, July-August, 2003.
15. Radulescu, M. I., and Hanson, R. K., "Effect of Heat Loss on Pulse-Detonation-Engine Flow Fields and Performance," Journal of Propulsion and Power, Vol. 21 (2), 2005, pp. 908-916.
16. Cooper, M., Jackson, S., Wintenberger, E., and Shepherd, J. E., "Direct Experimental Impulse Measurements for Detonations and Deflagrations," Journal of Propulsion and Power, Vol. 18, 2002, 1033-1041.
17. Cooper, M., and Shepherd, J. E., "Detonation Tube Impulse in Subatomospheric Environments," Journal of Propulsion and Power, Vol. 22, No. 4, 2006, pp. 845-851.
18. Morris, C. I., "Numerical Modeling of Single-Pulse Gasdynamics and Performance of Pulse Detonation Rocket Engines," Journal of Propulsion and Power, Vol. 21, 2005, pp. 527-538.
19. Matsuo, K., Compressible Flow Dynamics, Rikogakusha Publishing, 1994, pp. 200-233.
20. Japan Society of Mechanical Engineers, Flow Thermophysical Properties, 1983.