diff --git a/src/shared/algorithms/MEA/MEA.cpp b/src/shared/algorithms/MEA/MEA.cpp
index 399ee03ee6c06a36c2b8cd91e64af6f83215f895..8e1fcf93116ad7a569ce1336b9db82a5641b8b0d 100644
--- a/src/shared/algorithms/MEA/MEA.cpp
+++ b/src/shared/algorithms/MEA/MEA.cpp
@@ -190,4 +190,5 @@ void MEA::updateState()
     state.estimatedMass     = x(2);
     state.estimatedPressure = baroH * x;
     state.estimatedApogee   = apogee;
+    state.estimatedForce    = force;
 }
\ No newline at end of file
diff --git a/src/shared/algorithms/MEA/MEA.h b/src/shared/algorithms/MEA/MEA.h
index 56467767a1ca4bd22a51456129a62f42cdf42baf..0fa99d9d445d628ab2a9307056d20547d7ab35c6 100644
--- a/src/shared/algorithms/MEA/MEA.h
+++ b/src/shared/algorithms/MEA/MEA.h
@@ -59,7 +59,7 @@ public:
         Aeroutils::AerodynamicCoeff coeffs;  //< Aerodynamic coefficients.
         float crossSection;                  //< Cross section of the rocket.
 
-        float ae;  //< TODO: What is this?
+        float ae;  //< Efflux area
         float p0;  //< Pressure at nozzle exit
     };
 
diff --git a/src/shared/algorithms/MEA/MEAData.h b/src/shared/algorithms/MEA/MEAData.h
index 6164a8b7a9c2c1a85f8b5828e2128d653a66ce23..7358e242ae28b0f04c39768a1aacd93d84efa1f9 100644
--- a/src/shared/algorithms/MEA/MEAData.h
+++ b/src/shared/algorithms/MEA/MEAData.h
@@ -35,20 +35,23 @@ struct MEAState
     float estimatedPressure;
     float estimatedMass;
     float estimatedApogee;
+    float estimatedForce;
 
     float x0;
     float x1;
 
     static std::string header()
     {
-        return "timestamp,estimatedPressure,estimatedMass,estimatedApogee,x0,"
+        return "timestamp,estimatedPressure,estimatedMass,estimatedApogee,"
+               "estimatedForce,x0,"
                "x1\n";
     }
 
     void print(std::ostream &os) const
     {
         os << timestamp << "," << estimatedPressure << "," << estimatedMass
-           << "," << estimatedApogee << "," << x0 << "," << x1 << "\n";
+           << "," << estimatedApogee << "," << estimatedForce << "," << x0
+           << "," << x1 << "\n";
     }
 };