diff --git a/missions/2024_Lyra_Roccaraso_September/config/aerodynamicsConfig.m b/missions/2024_Lyra_Roccaraso_September/config/aerodynamicsConfig.m
new file mode 100644
index 0000000000000000000000000000000000000000..853f316298d13226b839c34f48a63ebb6012a6ea
--- /dev/null
+++ b/missions/2024_Lyra_Roccaraso_September/config/aerodynamicsConfig.m
@@ -0,0 +1,39 @@
+% CONFIG - This script sets up control parameters
+
+%% AERODYNAMICS DETAILS
+% These coefficients are obtained using MISSILE DATCOM, check simulator/README.md for further details.
+
+features = loadConfig("settingsConfig.m");
+
+if not(isfield(aerodynamics,'autoMatProt_flag')) || features.flags.autoMatProt
+    
+    % Coefficients
+    Coeffs = load(filename_coeffs);
+    aerodynamics.Coeffs = Coeffs.CoeffsTot;
+
+    % Geometry
+    aerodynamics.Geometry = Coeffs.Geometry;
+    aerodynamics.Geometry.xcg = Coeffs.Geometry.xcg';
+
+    % State
+    aerodynamics.State.Alphas = Coeffs.State.Alphas';
+    aerodynamics.State.Betas = Coeffs.State.Betas';
+    aerodynamics.State.Altitudes = Coeffs.State.Altitudes';
+    aerodynamics.State.Machs = Coeffs.State.Machs';
+    aerodynamics.State.Controls = Coeffs.State.hprot';
+    aerodynamics.State.xcgTime = Coeffs.State.xcgTime';
+    clear('Coeffs');
+
+    CoeffHighAOA = load('HighAOA.mat'); 
+    aerodynamics.highAOA.Coeffs = CoeffHighAOA.CoeffsTot; 
+    aerodynamics.highAOA.State.Alphas = CoeffHighAOA.State.Alphas';
+    aerodynamics.highAOA.State.Betas = CoeffHighAOA.State.Betas'; 
+    aerodynamics.highAOA.State.Altitudes = CoeffHighAOA.State.Altitudes'; 
+    aerodynamics.highAOA.State.Machs = CoeffHighAOA.State.Machs';
+    aerodynamics.highAOA.State.Controls = CoeffHighAOA.State.hprot';
+    aerodynamics.highAOA.State.xcgTime = CoeffHighAOA.State.xcgTime';
+    clear('CoeffHighAOA');
+
+    aerodynamics.highAOA.tb = aerodynamics.tb; 
+    aerodynamics.highAOA.timeEngineCut = aerodynamics.timeEngineCut; 
+end
\ No newline at end of file
diff --git a/missions/2024_Lyra_Roccaraso_September/config/engineConfig.m b/missions/2024_Lyra_Roccaraso_September/config/engineConfig.m
index b47c21709f71521a93c25e0c9b7b53bba7d8aad0..158e439b5dc9c131a1f7017d39b3dcebe2def5d3 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/engineConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/engineConfig.m
@@ -4,3 +4,5 @@ engine.name = 'HRE_FURIA-Rv2-T04T03';
 engine.burnTime = inf;                                 % [s] Burn duration
 engine.ignitionTime = 000; %0.4;                       % [s] Ignition transient
 engine.cutOffTime = 000; %0.3;                         % [s] Cut-off transient
+
+filename_coeffs = strcat(engine.name, '.mat');
\ No newline at end of file
diff --git a/missions/2024_Lyra_Roccaraso_September/config/settingsConfig.m b/missions/2024_Lyra_Roccaraso_September/config/settingsConfig.m
index 0044a9b1f191aae55e68f512bb8767af87764fb6..a6970da492a7046f7b695fb7b908b1b154e95a6b 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/settingsConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/settingsConfig.m
@@ -4,4 +4,6 @@
 % mission (e.g. whether a specific algorithm is used, the engine type, 
 % flags...)
 
-features.engineType = 'hybrid';      % [-] choices are: solid, hybrid
\ No newline at end of file
+settings.engineType = 'hybrid';      % [-] choices are: solid, hybrid
+
+settings.flags.autoMatProt = false;
\ No newline at end of file