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vMinLOF Element

Main element containing the results for take-off calculations optimized for min-imum liftoff speed VLOFmin

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
All All
      Element gammaCheck

Flight path angle being achieved at V2 with one engine failure in 400 ft height above ground. This is the result of a post trim calculation using the deter-mined V2. If the trim calculation fails the entry is set to -90.

      Element todV2

Take-off distance at safety speed V2

      Element todVLiftoff

Take-off distance at liftoff speed VLOF

      Element v1

Take-off decision speed V1

      Element v2

Safety speed V2

      Element vElevOptimal

Optimal speed Velev at point of initiating take-off rotation by elevator deflection for a minimum take-off distance

      Element vLiftoff

Liftoff speed VLOF

      Element vMCG

Minimum control speed ground VMCG

      Element vRotationOptimal

Optimal rotation speed VR for a mini-mum take-off distance

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string

Directory of the external data file

Attribute externalDataNodePathSimple Type string

Path of the node inside the external data file

Attribute externalFileNameSimple Type string

Name of the external data file

See Also