diff --git a/schema/cpacs_schema.xsd b/schema/cpacs_schema.xsd index 67ea802..d76547e 100644 --- a/schema/cpacs_schema.xsd +++ b/schema/cpacs_schema.xsd @@ -18323,7 +18323,7 @@ The fuel tank volume type should also be used for the wing fuel tank - massInertiaType + Mass intertia massInertiaType @@ -34708,6 +34708,7 @@ The fuel tank volume type should also be used for the wing fuel tankDescription + Contour: single or double @@ -34919,6 +34920,7 @@ The fuel tank volume type should also be used for the wing fuel tank + Number of trolleys @@ -35030,6 +35032,7 @@ The fuel tank volume type should also be used for the wing fuel tank + Number of seats @@ -35233,6 +35236,41 @@ The fuel tank volume type should also be used for the wing fuel tank + + + + + + + + + + + + + Mass + + + Description of mass, center of gravity and inertia + + + + + + + + + + + Mass value + + + + + Center of gravity (x,y,z) + + +