Using pressure- and temperature-sensitive paint for global surface pressure and temperature measurements on the aft-body of a capsule reentry vehicle

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Watkins, A Neal ^a   Buck, Gregory M ^a   Leighty, Bradley D ^a   Lipford, William E ^a   Oglesby, Donald M ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CREW MODULE; EFFECTIVE TOOL; MODEL SURFACE; PRESSURE SENSITIVE PAINTS; RE-ENTRY VEHICLES; REACTION CONTROL SYSTEM; SURFACE INTERACTIONS; SURFACE PRESSURES; SYSTEM DESIGN; TEMPERATURE SENSITIVE PAINT; TEMPERATURE-SENSITIVE; TESTING ENVIRONMENT;

AERODYNAMIC CONFIGURATIONS; AEROSPACE ENGINEERING; AUTOMOBILE BODIES; PAINT; REENTRY; TEMPERATURE MEASUREMENT;

SURFACE REACTIONS;

EID: 78149455184     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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