NASA General Aviation Crashworthiness Seat Development
Three load limiting seat concepts for general aviation aircraft designed to lower the deceleration of the occupant in the event of a crash were sled tested and evaluated with reference to a standard seat. Dummy pelvis accelerations were reduced up to 50 percent with one of the concepts. Computer pro...
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Published in: | SAE transactions Vol. 88; pp. 2075 - 2085 |
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Main Authors: | , |
Format: | Journal Article |
Language: | English |
Published: |
SOCIETY OF AUTOMOTIVE ENGINEERS, INC
01-01-1979
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Abstract | Three load limiting seat concepts for general aviation aircraft designed to lower the deceleration of the occupant in the event of a crash were sled tested and evaluated with reference to a standard seat. Dummy pelvis accelerations were reduced up to 50 percent with one of the concepts. Computer program MSOMLA (Modified Seat Occupant Model for Light Aircraft) was used to simulate the behavior of a dummy passenger in a NASA full-scale crash test of a twin engine light aircraft. A computer graphics package MANPLOT was developed to pictorially represent the occupant and seat motion. |
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AbstractList | Three load limiting seat concepts for general aviation aircraft designed to lower the deceleration of the occupant in the event of a crash were sled tested and evaluated with reference to a standard seat. Dummy pelvis accelerations were reduced up to 50 percent with one of the concepts. Computer program MSOMLA (Modified Seat Occupant Model for Light Aircraft) was used to simulate the behavior of a dummy passenger in a NASA full-scale crash test of a twin engine light aircraft. A computer graphics package MANPLOT was developed to pictorially represent the occupant and seat motion. |
Author | Alfaro-Bou, Emilio Fasanella, Edwin L. |
Author_xml | – sequence: 1 givenname: Edwin L. surname: Fasanella fullname: Fasanella, Edwin L. – sequence: 2 givenname: Emilio surname: Alfaro-Bou fullname: Alfaro-Bou, Emilio |
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ContentType | Journal Article |
Copyright | Copyright © Society of Automotive Engineers, Inc., 1980 |
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EndPage | 2085 |
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Snippet | Three load limiting seat concepts for general aviation aircraft designed to lower the deceleration of the occupant in the event of a crash were sled tested and... |
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StartPage | 2075 |
SubjectTerms | Aircraft Aircraft pitch Computer graphics Crashworthiness General aviation Light aircraft Passengers Pelvis Sleds Speed |
Title | NASA General Aviation Crashworthiness Seat Development |
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Volume | 88 |
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