Accession Number:

AD0699371

Title:

HELICOPTER EXTERNAL SLING SYSTEM BASIC VIBRATION DATA.

Descriptive Note:

Engineering rept.,

Corporate Author:

ARMY TRANSPORTATION ENGINEERING AGENCY FORT EUSTIS VA

Personal Author(s):

Report Date:

1969-12-01

Pagination or Media Count:

11.0

Abstract:

Simulated tests were conducted of helicopter externally slung loads ranging from 2,000 to 4,000 pounds on an analog computer. Author

Subject Categories:

  • Helicopters
  • Couplers, Fasteners and Joints

Distribution Statement:

APPROVED FOR PUBLIC RELEASE