Thrust modulation in a nitrous-oxide/hydroxyl-terminated polybutadiene hybrid rocket motor

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 3, Issue , 2006, Pages 1933-1944

  Rajesh, K K ^a,b  

^a Defense Research and Development Laboratory ^*  (India)

^b Solid Rocket and Solid Ramjet Propulsion Division   (India)

Author keywords

[No Author keywords available]

Indexed keywords

HYBRID ROCKET MOTOR; HYDROXYL TERMINATED POLYTOUTADIENE (HTPB); MASS FLOW; THRUST MODULATION;

CORRELATION METHODS; DATA ACQUISITION; LIQUID FUELS; NITROGEN COMPOUNDS; ORGANIC COMPOUNDS; REGRESSION ANALYSIS;

ROCKET ENGINES;

EID: 34249289715     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Krishnan, S., "Hybrid Rocket Technology: An Overview," Third International High Energy Materials Conference and Exhibit, Thiruvanthapuram, India, Dec.6-8, 2000, pp. 62-71.
2. 2O/HTPB Hybrid Rocket " from the web site of University of Colorado at Boulder, USA.
3. George, P., et al., "Fuel Regression Rate in Hydroxyl-Terminated- Polybutadiene/Gaseous Oxygen Hybrid Rocket Motors," Journal of Propulsion and Power, Vol. 17, No. 1, January-February, 2001, pp. 35-42.
4. Wemimont, E. J., and Heister, S. D., "Combustion Experiments in Hydrogen Peroxide/Polyethylene Hybrid Rocket with Catalytic Ignition," Journal of Propulsion and Power, Vol. 16, No. 2, March-April ,2000, pp. 318-325.
5. Gordon, S., and McBride, B. J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications," NASA Reference Publication 1311.
6. Freedman, E., " Thermodynamic Properties of Military Gun Propellants," in Stiefel, L., Gun Propulsion Technology, Ch.5, US Army Armament Research, Development and Engineering Center Picatinny Arsenal, N.J.