Pilot Harness Suspension Study

Abstract

Test manikins are used extensively to collect ejection test data in situations not appropriate for humans, but the accuracy of the manikin data is directly dependent on how well the test set-up simulates the actual pre-ejection conditions experienced by the pilot. The objective of this program was to investigate the differences in harness tension among pilots and to compare these tensions to those typically used in a test manikin in order to provide validation for data collected during manikin impact tests. Four pilots and one Hybrid III 50th percentile manikin were lifted off the ground with a suspension hoist where a series of harness tension measurements were taken. The results demonstrated large individual differences among the human subjects and between the humans and the test manikin in the amount of harness slack generated by the lifting. Recommendations were made for setting the harness side adjustment index at level three during future manikin tests.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 2004
Accession Number
ADA430990

Entities

People

  • Benjamin C. Kuennen
  • John R. Buhrman

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Air Force Research Laboratories
  • Ejection
  • Ejection Seats
  • Fighter Aircraft
  • Flight Crews
  • Government Procurement
  • Governments
  • Impact Acceleration
  • Measurement
  • Military Pilots
  • Military Research
  • Pilots
  • Shoulder
  • Technical Information Centers
  • United States

Fields of Study

  • Engineering

Readers

  • Aerospace Test and Evaluation
  • Aviation Science / Aeronautics.
  • Exercise and Sports Science.