Certified Ejection Seat Weight Ranges and their Effects on Personnel Selection
Human Systems Integration Capstone === Approved for public release; distribution is unlimited === Current ejection seat certified aircrew weight ranges (136 to 213 lbs.), such as for the F/A-18, prohibited over one third (38%) of women and (8%) of men from accessing the naval aviation strike pipelin...
Main Author: | Jones, Thomas C. |
---|---|
Other Authors: | Shattuck, Lawrence |
Language: | en_US |
Published: |
Monterey, California: Naval Postgraduate School.
2014
|
Subjects: | |
Online Access: | http://hdl.handle.net/10945/43804 |
Similar Items
-
The mathematical model of the pilot’s ejection process by using the K-36DM ejection seat
by: Kowaleczko Grzegorz, et al.
Published: (2018-12-01) -
Ispitivanje piropatrona i raketnog motora pilotskog sedišta / Testing pyrocartridges and the rocket motor of the ejection seat
by: Milorad Savković
Published: (2008-04-01) -
Modeling viscoelastic responses of the head/neck system during pilot ejection
by: Deuel, Christopher R.
Published: (2014) -
Predictors of aviation service selection among U.S. Naval Academy graduates
by: Gonzalez, James Mario
Published: (June) -
Heart failure with mid-range ejection fraction: Current evidence and uncertainties
by: Raffaele Martone, et al.
Published: (2019-04-01)