Nondestructive evaluation for the space shuttle's wing leading edge

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Madaras, Eric I ^a   Winfree, William P ^a   Prosser, William H ^a   Wincheski, Russell A ^a   Cramer, K Elliot ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON; COMPUTERIZED TOMOGRAPHY; EDDY CURRENT TESTING; ICE; IMPACT TESTING; NASA; ORBITS; PRINCIPAL COMPONENT ANALYSIS; PROPULSION; REINFORCEMENT; SPACE DEBRIS; SPACE PLATFORMS; SPACE SHUTTLES; ULTRASONIC APPLICATIONS; WINGS;

HIGH-RESOLUTION COMPUTED TOMOGRAPHY; MICROMETEOROID AND ORBITAL DEBRIS; NON DESTRUCTIVE EVALUATION; NON-DESTRUCTIVE EVALUATION METHODS; REINFORCED CARBON CARBONS; THERMAL PROTECTION SYSTEM; THERMOGRAPHIC DETECTION; WIRELESS ACCELEROMETERS;

ACOUSTIC EMISSION TESTING;

EID: 77957837599     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3630     Document Type: Conference Paper

References (1)

1. Gehman, H., Adm. USN, Chairman, Columbia Accident Investigation Boar Report, v3, US Gov. Printing Office document no. 033-000-01260-8, Aug. 2003.