This standard was last reviewed and confirmed in 2018. Therefore this version remains current.
Abstract Preview
The aircraft is assumed to be rigid, of constant mass and of constant inertia. It is not equipped with systems modifying its natural dynamic behaviour. However, most of the definitions can be applied to the case of a flexible aircraft, of variable mass and of variable inertia. The general concepts defined are applicable to the atmospheric flight phase.
General information
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Status : PublishedPublication date : 1992-06
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Edition : 1Number of pages : 8
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- ICS :
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Quantities and units
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Aircraft and space vehicles in general
Buy this standard
Format | Language | |
---|---|---|
Paper |
- CHF58
Life cycle
A standard is reviewed every 5 years
Revisions / Corrigenda
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Now confirmed
ISO 1151-8:1992 -
Revised by
ISO/CD 1151-8
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