diff --git a/classes/misc/Coefficient.m b/classes/misc/Coefficient.m
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+++ b/classes/misc/Coefficient.m
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+classdef Coefficient
+    % Motor: Manages the coefficients associated with a rocket
+    %
+    %   Constructor:
+    %       - Coefficient: Creates an instance of the Coefficient class.
+    %           Loaded config: -
+    %           Loaded data: aeroCoefficients.mat
+    %           Arguments:
+    %               - filePath: char, path to coefficient file to load
+    %               - name: (optional) coefficient name. Used when dynamic
+    %               derivatives are also needed
+    %
+    %   Coefficients are retrieved from DM in the following format:
+    %       Coefficient matrix: double (15, nAlpha, nMach, nBeta, nAlt, nAbk, nXcg) 
+    %       Where the 15 coefficients are 
+    %           - CA        Axial force 
+    %           - CYB       Side force derivative wrt beta
+    %           - CY0       Side force
+    %           - CNA       Normal force derivative wrt alpha
+    %           - CN0       Normal force
+    %           - Cl        Rolling moment
+    %           - Clp       Rolling moment derivative wrt roll rate
+    %           - Cma       Pitching moment derivative wrt alpha
+    %           - Cm0       Pitching moment
+    %           - Cmad      Pitching moment derivative wrt alpha dot
+    %           - Cmq       Pitching moment derivative wrt pitch rate
+    %           - Cnb       Yawing moment derivative wrt beta
+    %           - Cn0       Yawing moment
+    %           - Cnr       Yawing moment derivative wrt yaw rate
+    %           - Cnp       Yawing moment derivative wrt roll rate
+    %
+    %   NOTE: When dynamic derivatives are not loaded, the matrix will be
+    %   6-D, as there will be no need to interpolate wrt to the xcg: moment
+    %   transport formulas will be used instead
+
+    properties
+        static          % Static coefficients: [CA, CY, CN, Cl, Cm, Cn]
+        dynamic         % Dynamic derivatives: [Clp, Cmad, Cmq, Cnr, Cnp]
+
+        finsCN          % Fins-only CN
+        geometry        % Reference geometry
+        state           % Flight envelope
+    end
+
+    properties(Access = private)
+        loadDynamic     % Whether to load dynamic derivatives. Adds XCG dependece
+    end
+    
+    methods
+        function obj = Coefficient(filePath, name)
+            arguments
+                filePath    (1, :)  char
+                name        (1, :)  char = 'generic'
+            end
+            
+            obj = obj.loadData(filePath, name);
+        end
+    end
+
+    methods(Access = private)
+        function obj = loadData(obj, filePath, name)
+            % Load the coefficients from the specified file
+            % filePath: char, path to coefficient file to load
+            % name: (optional) coefficient name. Used when dynamic
+            % derivatives are also needed
+            %
+            % NOTE: Coefficient alpha and beta derivatives are not loaded
+            %       as coefficients are already interpolated linearly
+            
+
+            if ~exist(filePath, 'file'), return; end
+            warning('off'); % Disable warning in case coefficients are not present
+            dataCoeffs = load(filePath, name);
+            warning('on');
+            
+            if ~isfield(dataCoeffs, name), return; end
+            dataCoeffs = dataCoeffs.(name);
+
+            obj.loadDynamic = ~strcmp(name, 'generic');
+            obj.finsCN = dataCoeffs.finsCN;
+            obj.geometry = dataCoeffs.geometry;
+            obj.state = dataCoeffs.state;
+            
+            % Load CA, CY, CN, Cl, Cm, Cn
+            obj.static = dataCoeffs.total([1, 3, 5, 6, 9, 13], :, :, :, :, :, :);
+
+            if obj.loadDynamic
+                % Load Clp, Cmad, Cmq, Cnr, Cnp
+                obj.dynamic = dataCoeffs.total([7, 10, 11, 14, 15], :, :, :, :, :, :);
+            end
+        end
+    end
+end
+