Performance of a low density ablative heat shield material

Journal of Spacecraft and Rockets

Volumn 45, Issue 2, 2008, Pages 237-247

  Covington, M A ^a,d   Heinemann, J M ^a,d   Goldstein, H E ^b,d   Chen, Y K ^c   Terrazas Salinas, I ^c   Balboni, J A ^c   Olejniczak, J ^c,d   Martinez, E R ^c  

^a ELORET CORPORATION   (United States)

^b Research Institute for Advanced Computer Science   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ABLATIVE MATERIALS; AIRCRAFT MODELS; EARTH (PLANET); ITERATIVE METHODS; THERMODYNAMIC PROPERTIES;

ABLATIVE RECESSION RATES; ARC JET TESTS; STARDUST DESIGN;

HEAT SHIELDING;

EID: 42949090315     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.12403     Document Type: Conference Paper

References (14)