Modeling and experimental verification of auto-ignition processes for a green bi-propellant thruster

61st International Astronautical Congress 2010, IAC 2010

Volumn 6, Issue , 2010, Pages 4897-4911

  Schiebl, Markus ^a   Krejci, D ^a   Woschnak, A ^a   Winter, F ^b   Lang, M ^c   Scharlemann, C ^a  

^a AIT AUSTRIAN INSTITUTE OF TECHNOLOGY   (Austria)

^b VIENNA UNIVERSITY OF TECHNOLOGY   (Austria)

^c EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTICAL MODEL; AUTO-IGNITION; AUTO-IGNITION PROCESS; BI-PROPELLANT SYSTEM; CORRELATION FUNCTION; DEVELOPMENT TASKS; EUROPEAN SPACE AGENCY; EXPERIMENTAL SETUP; EXPERIMENTAL VERIFICATION; FLOW REACTORS; FUEL MIXTURES; GREEN PROPELLANTS; HEAT TRANSFER PROCESS; IGNITION CONDITIONS; IGNITION DELAYS; INITIAL CONDITIONS; INITIAL PRESSURE; MASS FLOW; MICRO-PROPULSION SYSTEMS; MIXTURE OF HYDROCARBONS; MODEL VALIDATION; NON-ADIABATIC; OPERATIONAL COSTS; PHYSICOCHEMICAL PARAMETERS; PRESSURE AND TEMPERATURE; PROPULSION SYSTEM; RESIDENCE TIME DISTRIBUTIONS; SPACE MISSIONS; SURFACE-TO-VOLUME RATIO; THERMAL IGNITION; THRUSTER SYSTEM;

CHEMICAL ANALYSIS; COMBUSTION CHAMBERS; ETHANOL; EXPLOSIVES; HYDROGEN; HYDROGEN PEROXIDE; IGNITION SYSTEMS; INERTIAL CONFINEMENT FUSION; INVESTMENTS; MATHEMATICAL MODELS; MIXTURES; OXIDATION; PROPELLANTS; REACTION KINETICS; SPACE FLIGHT; SPACECRAFT PROPULSION;

IGNITION;

EID: 79959426870     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Salome R, "The propulsion system of the CNES microsatellite product line", in Proc. 3rd Internat. Conf. On Spacecraft propulsion ESA SP-465, Dec. 2000, p. 99-105.
2. Cong Y., Zhang T., et. al., "Study on Kerosene based Fuel with Hydrogen Peroxide for Hypergolic Application", Proc. 2nd Int. Conference on Green Propellants for Space Propulsion, ESA SP-557
3. Scharlemann C., Schiebl M., Marhold K., Tajmar M., "Test of a Turbo-Pump Fed Miniature Rocket Engine", AIAA-2006-4551
4. Khan, Qasim Sawar, Baek, Seung Wook, Ghassemi Hojat, On the Auto ignition and Combustion Characteristics of Kerosene Droplets at Elevated Pressure and Temperatures, Combustion Science and Technology, 179:12, 2437-2451
5. Sadov V., "Ignition of Kerosene and Hydrogen Peroxide in Combustion Chamber by Fire Jet", Russian Scientific Center.
6. Forman A. Williams, "Combustion Theory", Perseus Books, 2nd Edition, 1985
7. N.N. Semenov, "Chemical Kinetics and Reactivity", vols. I and II, Princeton: Princeton University Press, 1958, 1959
8. D. A. Frank-Kamenetskii, "Diffusion and Heat Transfer in Chemical Kinetics", New York: Plenum Press, 1969
9. P.H. Thomas, C & F9, 369 (1965)
10. P. Gray and P. R. Lee, "Oxidation and Combustion Review" 2, 1(1967).
11. B. F. Gray and C. H. Yang, 11th Symp. (1967), 1057-1061
12. Schiebl M., "Evaluation of ignition conditions of a hydrogen peroxide based μ-Propulsion System", MS-Thesis, 2010
13. Rutherford Sris, "Vectors, Tensors, and the Basic Equations of Fluid Mechanics", Dover Publication, 1989
14. Turner, J.,M.,"Rocket and Spacecraft Propulsion: Principles, Practice and New Developments", Springer 3rd ed. 2008
15. Leonardi F., Larochette M., et al.," Optimisation of extruded polymer foam by the resident time distribution approach", Proceedings of the Polymer Processing Society 24th Annual Meeting
16. Walder, H., and Broughton, L.W., "Thermal Ignition Tests of Hydrogen Peroxide and Kerosine in a 22001b Thrust Rocket Motor," Royal Aircraft Establishment, RAE-TN-RPD-70, Aug. 1952.
17. Walder, H., "An Investigation into the Thermal Ignition of Hydrogen Peroxide and Kerosine," Royal Aircraft Establishment, RAE-R-RPD 7, May 1950.
18. Walder, H., "Further Investigations into the Thermal Ignition of Hydrogen Peroxide and Kerosine," Royal Aircraft Establishment, RAE-TNRPD-43, Dec. 1950.
19. Sisco J.C., et al. "Autoignition of Kerosene by Decomposed Hydrogen Peroxide in a Dump-Combustor Configuration", Journal of Propulsion and Power, Vol.21, No. 3, May-June 2005, pp. 450-459
20. Park, G., Lim H., "Novel Ramjet Propulsion System with H2O2-Kerosene Rocket as an Initial Accelerator", 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit 21-23 July 2008, Hartfort, CT
21. Vasu, S. S., Davidson, D. F., Hanson R. K., "Jet fuel delay times: Shock tube experiments over wide conditions and surrogate model predictions", Combustion and Flame 152 (2008) 125-143 (Pubitemid 351625146)
22. Dean, A. J., Penyazkov, O. G., Sevruk K. L., Varatharajan B., "Autoignition of surrogate fuels at elevated temperatures and pressures", Proceedings of the Combustion Institute 31 (2007) 2481-2488 (Pubitemid 47430507)