Accession Number:

ADA046279

Title:

Flight Test of a Composite Multi-Tubular Spar Main Rotor Blade on the AH-1G Helicopter. Volume II. Cost Estimates and Process Specifications.

Descriptive Note:

Final rept. Jun 74-Jan 77,

Corporate Author:

HUGHES HELICOPTERS CULVER CITY CALIF

Personal Author(s):

Report Date:

1977-08-01

Pagination or Media Count:

79.0

Abstract:

The objectives of this program were to design a composite main rotor blade in the multi-tubular spar configuration to be directly interchangeable in pairs with the production metal 540 blades on the AH-1G helicopter, have increased fatigue life, invulnerability to the 23mm ballistic threat, low radar cross section, and low fabrication cost. Manufacturing technology was developed and described in a Process Specification. Laboratory, ground, and flight tests demonstrated that the wet filament wound, co-cured blade met, and in some cases surpassed, all objectives and could be adapted for Army service. Author

Subject Categories:

  • Helicopters
  • Economics and Cost Analysis
  • Laminates and Composite Materials

Distribution Statement:

APPROVED FOR PUBLIC RELEASE