diff --git a/addContent/schema/v3_4_alicia/cpacs_schema.xsd b/addContent/schema/v3_4_alicia/cpacs_schema.xsd
index eaa6924a..ca38c2fb 100644
--- a/addContent/schema/v3_4_alicia/cpacs_schema.xsd
+++ b/addContent/schema/v3_4_alicia/cpacs_schema.xsd
@@ -3044,15 +3044,9 @@ cpacs@dlr.de
-
-
-
-
-
- Bada model designator
-
-
-
+
+
+
@@ -3162,6 +3156,33 @@ cpacs@dlr.de
+
+
+
+
+
+ Aircraft Type
+
+
+
+
+
+
+
+
+
+
+
+
+ Bada model designator
+
+
+
+
+
+
+
+
@@ -12685,6 +12706,99 @@ cpacs@dlr.de
+
+
+
+
+
+ Emission grids
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+ Emission grid
+
+
+
+
+
+
+
+
+
+ Name
+
+
+
+
+ Description
+
+
+
+
+ Latitude coordinate [0-360]
+
+
+
+
+ Longitude coordinate [0-360]
+
+
+
+
+ Altitude [m]
+
+
+
+
+ Fuel [kg]
+
+
+
+
+ CO2 mass [kg]
+
+
+
+
+ NOx mass [kg]
+
+
+
+
+ H20 mass [kg]
+
+
+
+
+ Distance [m]
+
+
+
+
+ Cell Distribution Factor [-]
+
+
+
+
+
+
+
+
@@ -12822,6 +12936,25 @@ cpacs@dlr.de
+
+
+
+
+
+ Energy Carriers
+
+
+
+
+
+
+
+
+
+
+
+
+
@@ -13595,6 +13728,74 @@ cpacs@dlr.de
+
+
+
+
+
+ Engine type
+
+
+
+
+
+
+
+
+
+
+ Engine concept (turboprop | turbofan | piston | turboshaft | electric)
+
+
+
+
+
+
+ Turbofan engine
+
+
+
+
+ Turboprop engine
+
+
+
+
+ Piston engine
+
+
+
+
+ Turboshaft engine
+
+
+
+
+ Electric engine
+
+
+
+
+
+
+
+
+ ICAO unique identifier (e.g., 01P08CM107; not to confuse with uID in CPACS!)
+
+
+
+
+
+
+ Engine model number (e.g., CFM56-5B6/3)
+
+
+
+
+
+
+
+
@@ -13868,6 +14069,7 @@ cpacs@dlr.de
+
@@ -14010,10 +14212,10 @@ cpacs@dlr.de
-
+
- Synthetic aviation fuel [kg]
+ Sustainable aviation fuel [kg]
@@ -15059,6 +15261,11 @@ cpacs@dlr.de
+
+
+ Reference to predefined energy carrier to be used for this flight (defined at cpacs/vehicles/energyCarriers)
+
+
@@ -15080,7 +15287,7 @@ cpacs@dlr.de
- Load factor
+ Payload load factor [-]
@@ -16149,9 +16356,6 @@ cpacs@dlr.de
Fuels
-
- fuelType containing data for fuels
-
@@ -16228,33 +16432,75 @@ cpacs@dlr.de
- Fuels
+ Fuel
-
- fuelType containing data for fuels
- Can be used as a catalog for different (liquid) fuel
- types
-
-
-
-
-
+
+
+ Name
+
+
+
+
+ Description
+
+
+
+
+ Type of energy carrier
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+ Lower heating value
+
+
+
+
+ Density at 15deg C
+
+
+
+
+ CO2 emission index
+
+
+
+
+ H2O emission index
+
+
+
+
+ N2 emission index
+
+
+
- at 15deg C
+ Energy specific cost
+
+
+
+
+ Freezing point
-
-
-
-
-
-
@@ -20346,6 +20592,45 @@ The fuel tank volume type should also be used for the wing fuel tank
+
+
+
+
+
+ Life cycle
+
+
+
+
+
+
+
+
+
+
+ Entry into service
+
+
+
+
+
+
+ End of production
+
+
+
+
+
+
+ End of life
+
+
+
+
+
+
+
+
@@ -28990,6 +29275,92 @@ The fuel tank volume type should also be used for the wing fuel tank
+
+
+
+
+
+ Propulsion Architecture
+
+
+
+
+
+
+
+
+
+
+
+ Powertrain (combustion | electric | hybridElectric | hydrogenElectric)
+
+
+
+
+
+
+ Combustion
+
+
+
+
+ Electric
+
+
+
+
+ Hybrid-electric (e.g., battery + kerosene)
+
+
+
+
+ Hydrogen-electric (e.g., battery + hydrogen, or only fuel cell)
+
+
+
+
+
+
+
+
+ Type of the energy carrier (kerosene | hydrogen | battery | keroseneBattery | hydrogenBattery)
+
+
+
+
+
+
+ Kerosene
+
+
+
+
+ Hydrogen
+
+
+
+
+ Battery
+
+
+
+
+ Kerosene and battery
+
+
+
+
+ hydrogen and battery
+
+
+
+
+
+
+
+
+
+
@@ -31556,6 +31927,7 @@ The fuel tank volume type should also be used for the wing fuel tank
+
@@ -34973,9 +35345,9 @@ The fuel tank volume type should also be used for the wing fuel tankDelay [s]
-
+
- Distance [m]
+ Flight distance [m]
@@ -35029,6 +35401,12 @@ The fuel tank volume type should also be used for the wing fuel tankSoot mass [kg]
+
+
+ Payload load factor [-]
+
+
+
@@ -35741,7 +36119,7 @@ The fuel tank volume type should also be used for the wing fuel tank
-
+
diff --git a/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd b/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd
index eaa6924a..ca38c2fb 100644
--- a/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd
+++ b/addContent/schema/v3_4_impactMonitor/cpacs_schema.xsd
@@ -3044,15 +3044,9 @@ cpacs@dlr.de
-
-
-
-
-
- Bada model designator
-
-
-
+
+
+
@@ -3162,6 +3156,33 @@ cpacs@dlr.de
+
+
+
+
+
+ Aircraft Type
+
+
+
+
+
+
+
+
+
+
+
+
+ Bada model designator
+
+
+
+
+
+
+
+
@@ -12685,6 +12706,99 @@ cpacs@dlr.de
+
+
+
+
+
+ Emission grids
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+ Emission grid
+
+
+
+
+
+
+
+
+
+ Name
+
+
+
+
+ Description
+
+
+
+
+ Latitude coordinate [0-360]
+
+
+
+
+ Longitude coordinate [0-360]
+
+
+
+
+ Altitude [m]
+
+
+
+
+ Fuel [kg]
+
+
+
+
+ CO2 mass [kg]
+
+
+
+
+ NOx mass [kg]
+
+
+
+
+ H20 mass [kg]
+
+
+
+
+ Distance [m]
+
+
+
+
+ Cell Distribution Factor [-]
+
+
+
+
+
+
+
+
@@ -12822,6 +12936,25 @@ cpacs@dlr.de
+
+
+
+
+
+ Energy Carriers
+
+
+
+
+
+
+
+
+
+
+
+
+
@@ -13595,6 +13728,74 @@ cpacs@dlr.de
+
+
+
+
+
+ Engine type
+
+
+
+
+
+
+
+
+
+
+ Engine concept (turboprop | turbofan | piston | turboshaft | electric)
+
+
+
+
+
+
+ Turbofan engine
+
+
+
+
+ Turboprop engine
+
+
+
+
+ Piston engine
+
+
+
+
+ Turboshaft engine
+
+
+
+
+ Electric engine
+
+
+
+
+
+
+
+
+ ICAO unique identifier (e.g., 01P08CM107; not to confuse with uID in CPACS!)
+
+
+
+
+
+
+ Engine model number (e.g., CFM56-5B6/3)
+
+
+
+
+
+
+
+
@@ -13868,6 +14069,7 @@ cpacs@dlr.de
+
@@ -14010,10 +14212,10 @@ cpacs@dlr.de
-
+
- Synthetic aviation fuel [kg]
+ Sustainable aviation fuel [kg]
@@ -15059,6 +15261,11 @@ cpacs@dlr.de
+
+
+ Reference to predefined energy carrier to be used for this flight (defined at cpacs/vehicles/energyCarriers)
+
+
@@ -15080,7 +15287,7 @@ cpacs@dlr.de
- Load factor
+ Payload load factor [-]
@@ -16149,9 +16356,6 @@ cpacs@dlr.de
Fuels
-
- fuelType containing data for fuels
-
@@ -16228,33 +16432,75 @@ cpacs@dlr.de
- Fuels
+ Fuel
-
- fuelType containing data for fuels
- Can be used as a catalog for different (liquid) fuel
- types
-
-
-
-
-
+
+
+ Name
+
+
+
+
+ Description
+
+
+
+
+ Type of energy carrier
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+ Lower heating value
+
+
+
+
+ Density at 15deg C
+
+
+
+
+ CO2 emission index
+
+
+
+
+ H2O emission index
+
+
+
+
+ N2 emission index
+
+
+
- at 15deg C
+ Energy specific cost
+
+
+
+
+ Freezing point
-
-
-
-
-
-
@@ -20346,6 +20592,45 @@ The fuel tank volume type should also be used for the wing fuel tank
+
+
+
+
+
+ Life cycle
+
+
+
+
+
+
+
+
+
+
+ Entry into service
+
+
+
+
+
+
+ End of production
+
+
+
+
+
+
+ End of life
+
+
+
+
+
+
+
+
@@ -28990,6 +29275,92 @@ The fuel tank volume type should also be used for the wing fuel tank
+
+
+
+
+
+ Propulsion Architecture
+
+
+
+
+
+
+
+
+
+
+
+ Powertrain (combustion | electric | hybridElectric | hydrogenElectric)
+
+
+
+
+
+
+ Combustion
+
+
+
+
+ Electric
+
+
+
+
+ Hybrid-electric (e.g., battery + kerosene)
+
+
+
+
+ Hydrogen-electric (e.g., battery + hydrogen, or only fuel cell)
+
+
+
+
+
+
+
+
+ Type of the energy carrier (kerosene | hydrogen | battery | keroseneBattery | hydrogenBattery)
+
+
+
+
+
+
+ Kerosene
+
+
+
+
+ Hydrogen
+
+
+
+
+ Battery
+
+
+
+
+ Kerosene and battery
+
+
+
+
+ hydrogen and battery
+
+
+
+
+
+
+
+
+
+
@@ -31556,6 +31927,7 @@ The fuel tank volume type should also be used for the wing fuel tank
+
@@ -34973,9 +35345,9 @@ The fuel tank volume type should also be used for the wing fuel tankDelay [s]
-
+
- Distance [m]
+ Flight distance [m]
@@ -35029,6 +35401,12 @@ The fuel tank volume type should also be used for the wing fuel tankSoot mass [kg]
+
+
+ Payload load factor [-]
+
+
+
@@ -35741,7 +36119,7 @@ The fuel tank volume type should also be used for the wing fuel tank
-
+