Test of an Electrohydraulic Digital Actuator for Advanced Missile Systems.

Abstract

This report describes the testing of a digital electrohydraulic stepper actuator developed by Bendix Systems Division under a previous Air Force R&D contract. The testing included calibration and 50 hours of durability cycling type tests. The actuator was designed for a stall torque of 2000-inch pounds at a 3000 psi differential pressure. A discussion of the problems encountered during this program and an inspection analysis of the actuator after testing are included in this report. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1980
Accession Number
ADA087274

Entities

People

  • Mark C. Twyman

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abrasives
  • Actuators
  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Control Systems
  • Government Procurement
  • Governments
  • Heat Treatment
  • Life Tests
  • Machining
  • Materials
  • Measurement
  • Particles
  • Test And Evaluation
  • Tool Steel
  • Valves

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Integrated Circuit Design and Technology.
  • Metallurgy