NASA General Aviation Crashworthiness Seat Development

790591

02/01/1979

Event
Business Aircraft Meeting and Exposition
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/790591
Pages
11
Citation
Fasanella, E., and Alfaro-Bou, E., "NASA General Aviation Crashworthiness Seat Development," SAE Technical Paper 790591, 1979, https://doi.org/10.4271/790591.
Additional Details
Publisher
Published
Feb 1, 1979
Product Code
790591
Content Type
Technical Paper
Language
English