diff --git a/missions/2024_Lyra_Roccaraso_September/config/geometryConfig.m b/missions/2024_Lyra_Roccaraso_September/config/geometryConfig.m
index d22fbebb25fbf20ce0505079e8634f42061ad52f..c1be047c6e37fac18b1af20139ae2902234eae5e 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/geometryConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/geometryConfig.m
@@ -5,13 +5,13 @@
 %% Boat-tail
 % The boat-tail is simulated as a trunc of cone with the major diameter
 % equal to the rocket one (settings.C)
-geometry.boat.Length = 000;                                       % [m] Boat-tail length
-geometry.boat.Diameter = 000;                                     % [m] Boat-tail base diameter
+geometry.boat.length = 000;                                       % [m] Boat-tail length
+geometry.boat.diameter = 000;                                     % [m] Boat-tail base diameter
 
 %% Rocket ogive and central body
 geometry.center.length = 000; %1.517;                             % [m] Central body length
 geometry.center.caliber = 000;                                          % [m] Caliber (Fuselage Diameter)
-geometry.center.crossSection = pi*geometry.C^2/4;                       % [m^2] Cross-sectional Surface
+geometry.center.crossSection = pi*geometry.center.caliber^2/4;                       % [m^2] Cross-sectional Surface
 
 geometry.nose.length = 000;                                       % [m] Nosecone Length
 geometry.nose.ogiveType = 'MHAACK';                                   % [-] Nosecone shape
diff --git a/missions/2024_Lyra_Roccaraso_September/config/inertiaConfig.m b/missions/2024_Lyra_Roccaraso_September/config/inertiaConfig.m
index ac8ca9cc955eb82a133c8fb905af2af6041cc96c..2ff12cf69bd7c592bde7ea48b31522f78c9ce41b 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/inertiaConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/inertiaConfig.m
@@ -12,9 +12,9 @@ inertia.rocket.Iyy = 12.07664659;                             % [kg*m^2] Inertia
 inertia.rocket.Izz = 12.07701314;                             % [kg*m^2] Inertia to z-axis
 
 %%% Inertias for engine only
-inertia.engine.Ixx = HREmotors(iMotor).Ixx;                            % [kg*m^2] Inertia to x-axis
-inertia.engine.Iyy = HREmotors(iMotor).Iyy;                            % [kg*m^2] Inertia to y-axis
-inertia.engine.Izz = HREmotors(iMotor).Izz;                            % [kg*m^2] Inertia to z-axis
+% inertia.engine.Ixx = HREmotors(iMotor).Ixx;                            % [kg*m^2] Inertia to x-axis
+% inertia.engine.Iyy = HREmotors(iMotor).Iyy;                            % [kg*m^2] Inertia to y-axis
+% inertia.engine.Izz = HREmotors(iMotor).Izz;                            % [kg*m^2] Inertia to z-axis
 
 % %%% Total inertias
 % inertia.Ixx = inertia.rocketIxx + engineIxx;
diff --git a/missions/2024_Lyra_Roccaraso_September/data/HREmotors.mat b/missions/2024_Lyra_Roccaraso_September/data/HREmotors.mat
new file mode 100644
index 0000000000000000000000000000000000000000..1ffa2dbb3d70ca3e4350f7c90acc37ec7549e8ee
--- /dev/null
+++ b/missions/2024_Lyra_Roccaraso_September/data/HREmotors.mat
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:fbb0e6fb46b31cadbc084461987aa8f45d9128c7e6b8d59483b88809e1495f3f
+size 6730820