Heavy Lift Helicopters

Abstract

The bibliography contains unclassified references on heavy lift helicopters with a minimum payload of about 9,000 pounds or a minimum gross weight of 17,000 pounds. These references relate to rotor characteristics, rotor systems, rotor loads, lift propulsion, payloads, heavy lift rotors, configurations, design, and performance capabilities of the heavy lift helicopters. Computer-generated indexes of corporate author-monitoring agency, subject, personal author, and title are included.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1972
Accession Number
AD0740900

Entities

Organizations

  • Defense Technical Information Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Aviation Accidents
  • Control Systems
  • Gas Turbines
  • Helicopter Engines
  • Helicopter Rotors
  • Helicopters
  • Mechanics
  • Rotary Wing Aircraft
  • Test And Evaluation
  • Turbines
  • Turbojet Engines
  • Warning Systems

Readers

  • Aerodynamics.
  • Library and Information Science
  • Marine Hydrodynamics