Accession Number:

AD0857635

Title:

Accelerated Test Technology/Test Program.

Descriptive Note:

Final technical rept. Feb 68-Apr 69,

Corporate Author:

HUGHES AIRCRAFT CO FULLERTON CA GROUND SYSTEMS GROUP

Personal Author(s):

• Wojciechowski, Frank X.
• Gongwer, James C.

Report Date:

1969-07-01

Pagination or Media Count:

257.0

Abstract:

The report describes the methodology, implementation, statistical analysis, and results of the accelerated test technologytest program for nonelectronic parts. The program was comprised of three principal elements Accelerated life tests for miniature snap action switches and crystal can relays Fatigue life tests on magnesium bell cranks and Wear life tests on automobile engine cams and followers. Author

Descriptors:

• *HELICOPTER ROTORS
• *STRUCTURAL COMPONENTS
• ENGINE COMPONENTS
• MATHEMATICAL MODELS
• ACCELERATED TESTING
• ELECTRIC SWITCHES
• ELECTRIC RELAYS
• FATIGUE(MECHANICS)
• WEAR RESISTANCE
• CAMS
• SUBMINIATURE ELECTRICAL EQUIPMENT
• MATHEMATICAL PREDICTION
• FAILURE(MECHANICS)

Subject Categories:

• Helicopters
• Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE