<?xml version="1.0" encoding="utf-8"?>
<cpacs>
  <vehicles uID="AGILE_DC1_vehicleID">
    <aircraft>
      <model uID="agile_v13_modelID">
        <wings>
          <wing symmetry="x-z-plane" uID="MainWing_wingID">
            <referenceValues>
                  <aerodynamicCoefficients>
                    <CL>1.109600</CL>
                    <CD>NaN</CD>
                  </aerodynamicCoefficients>
            </referenceValues>
          </wing>
        </wings>
        <reference><area>82.648078</area></reference>
        <analyses>
          <loadAnalysis>
          <loadCases>
          <flightLoadCases>
          <flightLoadCase uID="Design-point_1.0g_MTOM_Vcr_cruiseHeight">
                  <state>
                    <atmosphericConditions>
                      <density>0.31093</density>
                    </atmosphericConditions>
                    <attitudeAndMotion>
                      <translation>
                        <velocity>
                          <u>230.178</u>
                        </velocity>
                      </translation>
                    </attitudeAndMotion>
                  </state>
                </flightLoadCase>
              </flightLoadCases>
            </loadCases>
          </loadAnalysis>
          <massBreakdown>
            <designMasses>
              <mTOM>
                <mass>45045.8583098</mass>
              </mTOM>
            </designMasses>
          </massBreakdown>
        </analyses>
        <global>
          <performanceTargets>
            <cruiseMach>
              <required>0.78</required>
            </cruiseMach>
            <initialCruiseAltitude>
              <required>12000</required>
            </initialCruiseAltitude>
          </performanceTargets>
          <designRange>
            <required unit="m">3500000</required>
          </designRange>
        </global>
      </model>
    </aircraft>
  </vehicles>
  <toolspecific>
    <sMFA>
      <modelUID>agile_v13_modelID</modelUID>
      <wingUID>MainWing_wingID</wingUID>
      <flightLoadCaseUID>Design-point_1.0g_MTOM_Vcr_cruiseHeight</flightLoadCaseUID>
      <specificFuelConsumption unit="N/Ns">1.8639e-004</specificFuelConsumption>
      <fuelFractionFactor unit="-">0.938</fuelFractionFactor>
      <dragForceWinglessAircraft unit="N">50000</dragForceWinglessAircraft>
    </sMFA>
  </toolspecific>
</cpacs>
