rotorcraftMassBreakdownType Complex Type |
massBreakdownType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
All | ||
designMasses | Design masses | |
fuel | Fuel mass | |
mOEM | Operating empty mass | |
payload | Payload mass |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |
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.