complexType · extension complexBaseType · all
Rotorcraft mass breakdown
The massBreakeDown is subdivided in designMasses, fuel, payload and mOME (operating empty mass).
designMass
The design mass is a description from TLARs and can be understand as design criteria.
fuel and payload
The fuel and payload mass are the maximum masses which can be achieved. Full fuel tanks, all passengers on board and full cargo holding.
mOEM
The operation empty mass structure is based on the Airbus Mass Standard brake down [AIRBUS MASS STANDARD 2008]. The operator’s mass empty (OME) is defined by the sum of the following component masses:
Each sub component has the following massDescription which include a:
That massdescription can be found at the designMasses direct under each item. At the fuel, payload and mOME under massDescription in each item and sub item.
For the clean up the mOME there is consisting a script witch is programmed in Matlab but also as standalone vision available. Setting for that tool can be done under toolspesifics/cmu.
| Name | Type | Constraints | Use | Default | Description |
|---|---|---|---|---|---|
@externalDataDirectory | xsd:string | optional | Directory of the external data file | ||
@externalDataNodePath | xsd:string | optional | Path of the node inside the external data file | ||
@externalFileName | xsd:string | optional | Name of the external data file |
| Name | Type | Constraints | OccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration. | Default | Description |
|---|---|---|---|---|---|
| allThe children below may appear in any order. Each may appear at most once. | |||||
designMasses | designMassesType | [1..1] required | Design masses | ||
payload | mPayloadType | [1..1] required | Payload mass | ||
fuel | mFuelType | [1..1] required | Fuel mass | ||
mOEM | rotorcraftMassOEMType | [1..1] required | Operating empty mass | ||
| Type | Name |
|---|---|
rotorcraftAnalysesType | massBreakdown |