Ablation characteristic of 3D C/SiC composite nozzle in a small solid rocket motor

Wuji Cailiao Xuebao/Journal of Inorganic Materials

Volumn 23, Issue 5, 2008, Pages 938-944

  Chen, Bo ^a   Zhang, Li Tong ^a   Cheng, Lai Fei ^a   Luan, Xin Gang ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Ablation; Ablation mechanisms; C SiC composites; Solid rocket motor

Indexed keywords

CARBON FIBER REINFORCED PLASTICS; COMBUSTION; MOTORS; NOZZLES; PROPELLANTS; ROCKET ENGINES; ROCKETS; SOLID PROPELLANTS;

ABLATION MECHANISMS; ABLATION PROPERTIES; C/SIC COMPOSITES; COMBUSTION GASES; HOT-FIRING; LINEAR ABLATION RATE; MASS ABLATION; SOLID ROCKET MOTOR; SOLID-PROPELLANT ROCKET MOTORS;

ABLATION;

EID: 54749142058     PISSN: 1000324X     EISSN: None     Source Type: Journal    
DOI: 10.3724/SP.J.1077.2008.00938     Document Type: Article

References (18)

1. Hlratzer A, Pfeiffer H. SAMPE, 2002, 38 (4): 22-29.
2. Papenburg U, Beyer S, Laube H. Advanced ceramic matrix composites for space propulsion systems. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 33rd, Seattle, WA, USA. AIAA-1997-3391.
3. Beyer S, Knabe H. Development and testing of C/SiC components for liquid rocket propulsion applications. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 35th, Los Angeles, CA, USA, 1999. AIAA-1999-2896.
4. Felix F, William F, Nancy R. An innovative thermal management system for a mach 4 to mach 8 hypersonic scramjet engine. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 34th, Cleveland, OH, USA, 1998. AIAA-1998-3734.
5. Siebenhaar A, Johnson R W. Aero jet storable fuel scramjet flow path concepts: phase I program overview. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 9th, Norfolk, VA, USA, 1999. AIAA-1999-4923.
6. Xu Y D, Zhang L T. J. Am. Ceram. Soc., 1997, 80 (7): 1897-1900.
7. Xu Y D, Zhang L T, Cheng L F, et al. Carbon, 1998, 36 (7-8): 1051-1056.
8. Sanford Gordon, Bonnie J McBride. Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications I. Analysis, NASA RP-1311. Cleveland, Ohio, USA. National Aeronautics and Space Administration, Lewis Research Center, 1994. 1-61.
9. Sanford Gordon, Bonnie J McBride. Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications II. User's Manual and Program Description, NASA RP-1311-P2. Cleveland, Ohio, USA. National Aeronautics and Space Administration, Lewis Research Center, 1996. 1-178.
10. Yu Daimon, Akiko Matsuo. Heat Flux Estimation on the Nozzle Wall of Solid Rocket Motor Nozzle, 23rd International Symposium on Space Technology and Science. Yokohama, JAPAN, 2002. ISTS 2002-e-05.
11. Nathan S. Jacobson. J. Am. Ceram. Soc., 1993, 76 (1): 3-28.
12. René C J Schiepers, van Frans J J Loo, de Gijsbertus With. J. Am. Ceram. Soc., 1988, 71 (6): C284-C287.