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Volumn 24, Issue 9, 2005, Pages 993-1007

Design of ablative liners for high heat and erosive conditions

Author keywords

Ablation; Carbon phenolic; Charring; Graphite; Nozzle

Indexed keywords

ABLATION; COMPOSITE MATERIALS; EROSION; GRAPHITE; HEAT FLUX; HEAT TREATMENT; INSULATING MATERIALS; MATHEMATICAL MODELS; MELTING; NOZZLES; OXIDATION;

EID: 23244452057     PISSN: 07316844     EISSN: None     Source Type: Journal    
DOI: 10.1177/0731684405048202     Document Type: Article
Times cited : (6)

References (11)
  • 1
    • 0026711906 scopus 로고
    • High temperature thermomechanical behavior of carbon-phenolic and carbon-carbon composites, I. analysis
    • McManus, H. L. N. and Springer, G. S. (1992). High Temperature Thermomechanical Behavior of Carbon-Phenolic and Carbon-Carbon Composites, I. Analysis, Journal of Composite Materials, 26(2): 206-229.
    • (1992) Journal of Composite Materials , vol.26 , Issue.2 , pp. 206-229
    • McManus, H.L.N.1    Springer, G.S.2
  • 2
    • 0023327253 scopus 로고
    • A mathematical model to predict the thermal response of decomposing expanding composite
    • Henderson, J. B. and Wieck, E. (1987). A Mathematical Model to Predict the Thermal Response of Decomposing Expanding Composite, Journal of Composite Materials, 21: 373-393.
    • (1987) Journal of Composite Materials , vol.21 , pp. 373-393
    • Henderson, J.B.1    Wieck, E.2
  • 3
    • 23244449663 scopus 로고
    • Analysis of charring ablation with description of associated computing program
    • Matting, F. W. (1970). Analysis of Charring Ablation with Description of Associated Computing Program, NASA TN D-6085.
    • (1970) NASA TN D-6085
    • Matting, F.W.1
  • 4
    • 17144374807 scopus 로고
    • An analysis of the coupled chemically reacting boundary layer and charring ablator - Part II - Finite difference solution for the in-depth response of charring materials considering surface chemical and energy balance
    • Moyer, C. B. and Rindal, R. A. (1968). An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator - Part II - Finite Difference Solution for the In-depth Response of Charring Materials Considering Surface Chemical and Energy Balance, NASA CR-1061.
    • (1968) NASA CR-1061
    • Moyer, C.B.1    Rindal, R.A.2
  • 5
    • 0002445638 scopus 로고
    • A simple equation for rapid estimation of rocket nozzle heat transfer coefficient
    • Bartz, D. R. (1957). A Simple Equation for Rapid Estimation of Rocket Nozzle Heat Transfer Coefficient, Jet Propulsion, 27: 49-51
    • (1957) Jet Propulsion , vol.27 , pp. 49-51
    • Bartz, D.R.1
  • 6
    • 23244447005 scopus 로고
    • Course notes on solid rocket propulsion
    • HT Madras, India
    • Course Notes on Solid Rocket Propulsion (1988). Short Term Course, HT Madras, India.
    • (1988) Short Term Course
  • 7
    • 85003301276 scopus 로고
    • Mechanical and chemical contributions to the erosion rates of graphite throats in rocket motor nozzles
    • Gowarikar, V. R. (1966). Mechanical and Chemical Contributions to the Erosion Rates of Graphite Throats in Rocket Motor Nozzles, Journal of Spacecrafts and Rockets, 3(10): 1490-1494.
    • (1966) Journal of Spacecrafts and Rockets , vol.3 , Issue.10 , pp. 1490-1494
    • Gowarikar, V.R.1
  • 9
    • 0036277040 scopus 로고    scopus 로고
    • Thermal response and ablation characteristics of carbon fiber reinforced composite with novel silicon containing polymer MSP
    • Ogasawara, T. (2002). Thermal Response and Ablation Characteristics of Carbon Fiber Reinforced Composite with Novel Silicon Containing Polymer MSP, Journal of Composite Materials, 36(2): 143-157.
    • (2002) Journal of Composite Materials , vol.36 , Issue.2 , pp. 143-157
    • Ogasawara, T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.