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Tests, Impact, Shock Absorber Landing Gear, Aircraft
- Aerospace Standard
Published December 05, 2007 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the resulting test report. It is intended to standardize impact test procedures on landing gear shock absorbers and to provide sufficient data to allow evaluation of the design with respect to requirements of MIL-L-8552 and MIL-S-8959 as applicable.
|Aerospace Standard||Direction Instrument, Non-Magnetic, Stabilized Type (Directional Gyro)|
|Ground Vehicle Standard||Airbag Module Deployment Test Procedure|
|Technical Paper||Crashworthy Design Considerations for General Aviation Seats|
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE I||Design landing tests|
|TABLE II||Miscellaneous landing tests|
|TABLE III||Landing tests|
|TABLE IV||Reserve energy tests|
|Unnamed Dataset 6|
|MIL-A-8860||This document is not part of the subscrption.|
|MIL-A-8863||This document is not part of the subscrption.|
|MIL-A-8868||This document is not part of the subscrption.|
|MIL-L-8552||This document is not part of the subscrption.|
|MIL-S-8698||This document is not part of the subscrption.|
|MIL-S-8959||This document is not part of the subscrption.|
|MIL-STD-831||This document is not part of the subscrption.|
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