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Burrell O. French
Article Category: Research Article
Volume/Issue: Volume 38: Issue 7
Online Publication Date: Jul 01, 1967
DOI:
Page Range: 719 – 722
M. M. Cohen,
R. J. Crosbie, and
L. H. Blackburn
Article Category: Research Article
Volume/Issue: Volume 44: Issue 1
Online Publication Date: Jan 01, 1973
DOI:
Page Range: 37 – 39
B. K. BohnkerM.D., M.P.H.,
E. F. FeeksM.D., and
G. McewenM.D., M.S.
Article Category: Research Article
Volume/Issue: Volume 64: Issue 10
Online Publication Date: Oct 01, 1993
DOI:
Page Range: 939 – 940
Francesco Feletti,
Andrea Aliverti,
Maggie Henjum,
Marco Tarabini, and
Eric Brymer
Article Category: Research Article
Volume/Issue: Volume 88: Issue 11
Online Publication Date: Nov 01, 2017
Page Range: 1016 – 1023
Disorienting Effects of Aircraft Catapult Launchings: III. Cockpit Displays and Piloting Performance
Malcolm M. Cohen
Article Category: Research Article
Volume/Issue: Volume 48: Issue 9
Online Publication Date: Sep 01, 1977
DOI:
Page Range: 797 – 804
Raymond P. Stowe,
Deborah L. Yetman,
William F. Storm,
Clarence F. Sams, and
Duane L. Pierson
Article Category: Research Article
Volume/Issue: Volume 79: Issue 2
Online Publication Date: Feb 01, 2008
Page Range: 117 – 122
Malcolm M. Cohen
Article Category: Research Article
Volume/Issue: Volume 47: Issue 1
Online Publication Date: Jan 01, 1976
DOI:
Page Range: 39 – 41
J. P. BagianM.D., P.E. and
L. E. SchaferM.S.E.
Article Category: Research Article
Volume/Issue: Volume 63: Issue 7
Online Publication Date: Jul 01, 1992
DOI:
Page Range: 624 – 628
Phillip A. BishopEd.D.,
Stuart M. C. LeeM.S.,
Nadine E. ConzaM.S.,
Lisa L. ClappM.A.,
Alan D. Moore Jr.Ph.D.,
W. Jon WilliamsPh.D.,
Mark E. GuilliamsM.A., and
Michael C. GreenisenPh.D.
Article Category: Research Article
Volume/Issue: Volume 70: Issue 7
Online Publication Date: Jul 01, 1999
DOI:
Page Range: 656 – 665
Rebecca S. Blue,
Karen M. Ong,
Kristi Ray,
Anil Menon,
Jaime Mateus,
Serena Auñón-Chancellor,
Ronak Shah, and
William Powers
Fig. 3.
Abort vehicle profile. Run 5 was designed to simulate a capsule launch with activation of a launch escape system (LES). Subjects experienced a rapid +Gx acceleration (maximum +3.3 Gx, onset rate +1 G · s−1) during the launch escape followed by a “loft” period of +1 Gx before descent acceleration of maximum +1.9 Gx (onset rate <0.5 G · s−1). The loft is followed by transient acceleration (including brief inversion, maximum –0.7 Gz) representing parachute deployment and splashdown, then a sinusoidal waveform representing capsule motion on water.