Test Pilot Evaluation of a Reclined Cockpit Seat as an Aid to G Tolerance and Performance
Abstract
Twenty-two student test pilots have participated in closed-loop tracking indoctrination runs on the Dynamic Environment Simulator. Each pilot flew through a series of profiles up to 6 G in both the conventional upright seat position and a 55 degrees tilt back seat position. The subjective responses and pilot questionnaires are presented.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1976
- Accession Number
- ADA025784
Entities
People
- John W. Frazier
- Kenneth W. Mcelreath
Organizations
- Air Force Research Laboratory