Preparation and Properties of PICA-X Before and After Carbonization
Author:
Affiliation:

(State Key Laboratory of Chemical Engineering, East China University of Science and Technology,Shanghai 200237)

Clc Number:

TB332

  • Article
  • | |
  • Metrics
  • |
  • Reference [8]
  • |
  • Related [20]
  • |
  • Cited by [0]
  • | |
  • Comments
    Abstract:

    Phenolic impregnated ceramic ablator (PICA-X) were prepared by impregnation of novolac phenolic resin solutions into mullite fiber mat, followed by so-gel reaction and ambient drying. The density of the PICA-X could be adjusted in a range of 0.45 to 0.50 g/cm3 by using different concentrations of novolac phenolic resin solutions. The microstructure, mechanical property, thermal insulation property and thermal stability of PICA-X before and after carbonization were systematically investigated. PICA-X, which are composed of phenolic aerogel reinforced by mullite fiber, exhibit excellent mechanical strength of 26.7 to 34.0 MPa and low thermal conductivity of 36 to 40 mW/(m·K). After carbonization at 1 000℃, the flexural strength and thermal conductivity of the resulting C-PICA-X are 13.9 to 14.5 MPa and 41 to 45 mW/(m·K), respectively. In addition, PICA-X exhibits good oxidation resistance before and after carbonization.

    Reference
    [1] LAUB B,VENKATAPATHY E.Planetary Probe Atmospheric Entry and Descent Trajectory Analysis and Science,October 6-9,3[C].Netherlands:ESA Publications Division,2004.
    [2] TRAN H,JOHNSON C,RASKY D,et al.31st Thermophysics Conference,June 17-20,6[C].Reston:American Institute of Aeronautics and Astronautics,1996.
    [3] TRAN H,JOHNSON C,HSU M T,et al.32nd Thermophysics Conference, June 23-25,7[C].Reston:American Institute of Aeronautics and Astronautics,1997.
    [4] WILLCOCKSON W H.Stardust sample return capsule design experience[J].Journal of Spacecraft and Rockets,1999,6(3):470-474.
    [5] MILOS F S,CHEN Y K.Ablation and thermal response property model validation for phenolic impregnated carbon ablator[J].Journal of Spacecraft and Rockets, 2010,7(5):786-805.
    [6] JOHNSON S M,GASCH M J,LEISER D,et al.15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, April 28-May 1,8[C].Reston:American Institute of Aeronautics and Astronautics,2008.
    [7] NOWLIN S,THIMONS L.Surviving the heat:the application of phenolic impregnated carbon ablators[C/OL].(2013-02-01)[2016-02-26].http://136.142.82.187/eng12/history/spring2013/pdf/3131.pdf.
    [8] 贾献峰,刘旭华,乔文明,等.酚醛浸渍碳烧蚀体(PICA)的制备、结构及性能[J].宇航材料工艺,2016,6(1):77-80.
    Comments
    Comments
    分享到微博
    Submit
Get Citation
Related Videos

Share
Article Metrics
  • Abstract:2807
  • PDF: 6243
  • HTML: 168
  • Cited by: 0
History
  • Received:March 14,2016
  • Revised:March 14,2016
  • Online: December 28,2016
Article QR Code