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Volumn 16, Issue 3, 2002, Pages 432-439

Response of heatshield material at stagnation point of Pioneer-Venus probes

Author keywords

[No Author keywords available]

Indexed keywords

ABLATION; FRICTION; HEAT CONDUCTION; PYROLYSIS; SPACE PROBES; THERMOCOUPLES;

EID: 0036638373     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/2.6697     Document Type: Article
Times cited : (68)

References (30)
  • 11
    • 0005534817 scopus 로고
    • Effect of improvements and uncertainties in thermophysical properties on carbon phenolic heatshield thermal performance predictions
    • June
    • (1977) AIAA Paper , vol.77 , Issue.787
    • Bueche, J.F.1
  • 19
  • 25
    • 84953415982 scopus 로고
    • Hybrid integral/quasi-steady solution of charting ablation
    • June
    • (1990) AIAA Paper , vol.90 , Issue.1677
    • Potts, R.L.1
  • 28
    • 0342521297 scopus 로고
    • An experimental study of a carbon-phenolic ablation material
    • Sept.
    • (1970) NASA TN , vol.D-5930
    • Sutton, K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.