Nitrous oxide hybrid rocket motor fuel regression rate characterization

Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Volumn 4, Issue , 2007, Pages 3485-3496

  Doran, Eric ^a,c,d   Dyer, Jonny ^a,d,e   Lohner, Kevin ^a,d,e   Dunn, Zachary ^a,c,d   Cantwell, Brian ^a,c,d   Zilliac, Greg ^b,d  

^a STANFORD UNIVERSITY   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c 496 Lomita Mall   (United States)

^d AIAA   (United States)

^e Stanford University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT FUELS; COMBUSTORS; HIGH DENSITY POLYETHYLENES; NITROGEN OXIDES;

AXIAL VARIATION; HYBRID ROCKET MOTORS; HYDROXYL TERMINATED POLYBUTADIENE (HTPB); NITROUS OXIDE;

ROCKET ENGINES;

EID: 36749086509     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-5352     Document Type: Conference Paper

References (4)

1. Lohner, K., Dyer, J., Doran, E., Dunn, Z., and Zilliac, G., "Fuel Regression Rate Characterization Using a Laboratory Scale Nitrous Oxide Hybrid Propulsion System," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA, Sacramento, CA, July 2006.
2. Boardman, T. A., Brinton, D. H., Carpenter, R. L., and Zoladz, T. F., "An Experimental Investigation of Pressure Oscillations and Their Suppression in Subscale Hybrid Rocket Motors," 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA, San Diego, CA, July 1995.
3. Marxman, G. A., Wooldridge, C. E., and Muzzy, R. J., "Fundamentals of Hybrid Boundary Layer Combustion," Progress in Aeronautics and Astronautics, Vol. 15, 1964, pp. 485-522.
4. Karabeyoglu, M. A., Cantwell, B. J., and Zilliac, G., "Development of Scalable Space-time Averaged Regression Rate Expressions for Hybrid Rockets," 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA, Tucson, AZ, July 2005.