ISO/TC 20/SC 8
| Projekta Nr. | ISO 1151-8:1992 |
|---|---|
| Nosaukums | <p>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.</p> |
| Reģistrācijas numurs (WIID) | 5716 |
| Darbības sfēra | <p>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.</p> |
| Statuss | Atcelts |
| ICS grupa | 01.060 49.020 |