Particle impact risk assessment for ablative thermal protection systems

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Naughton, Jonathan W ^a,b   Venkatapathy, Ethiraj ^a   Loomis, Mark P ^c  

^a Thermosciences Institute   (United States)

^b UNIVERSITY OF WYOMING   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; REENTRY; VEHICLES;

ANALYSIS METHOD; ANALYSIS TECHNIQUES; COMPUTATIONAL FLUID DYNAMICS SIMULATIONS; PARTICLE CHARACTERISTICS; PARTICLE IMPACT; RE-ENTRY VEHICLES; THERMAL PROTECTION MATERIAL; THERMAL PROTECTION SYSTEM;

RISK ASSESSMENT;

EID: 84982318974     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-166     Document Type: Conference Paper

References (12)

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