diff --git a/src/physics.cpp b/src/physics.cpp
index 77d18aa..6258c8e 100644
--- a/src/physics.cpp
+++ b/src/physics.cpp
@@ -58,56 +58,6 @@ Vec3 calculate_acceleration(Vec3 force, double mass) {
     return {0.0, 0.0, 0.0};
 }
 
-void rk4_step(Vec3* position, Vec3* velocity, double dt,
-              double body_mass, double parent_mass) {
-    Vec3 k1_vel, k2_vel, k3_vel, k4_vel;
-    Vec3 k1_pos, k2_pos, k3_pos, k4_pos;
-
-    Vec3 pos0 = *position;
-    Vec3 vel0 = *velocity;
-
-    k1_vel = evaluate_acceleration(pos0, body_mass, parent_mass);
-    k1_pos = vel0;
-
-    Vec3 pos1 = vec3_add(pos0, vec3_scale(k1_pos, dt * 0.5));
-    Vec3 vel1 = vec3_add(vel0, vec3_scale(k1_vel, dt * 0.5));
-    k2_vel = evaluate_acceleration(pos1, body_mass, parent_mass);
-    k2_pos = vel1;
-
-    Vec3 pos2 = vec3_add(pos0, vec3_scale(k2_pos, dt * 0.5));
-    Vec3 vel2 = vec3_add(vel0, vec3_scale(k2_vel, dt * 0.5));
-    k3_vel = evaluate_acceleration(pos2, body_mass, parent_mass);
-    k3_pos = vel2;
-
-    Vec3 pos3 = vec3_add(pos0, vec3_scale(k3_pos, dt));
-    Vec3 vel3 = vec3_add(vel0, vec3_scale(k3_vel, dt));
-    k4_vel = evaluate_acceleration(pos3, body_mass, parent_mass);
-    k4_pos = vel3;
-
-    Vec3 k_vel_sum = vec3_add(vec3_add(k1_vel, vec3_scale(k2_vel, 2.0)),
-                              vec3_add(vec3_scale(k3_vel, 2.0), k4_vel));
-    Vec3 k_pos_sum = vec3_add(vec3_add(k1_pos, vec3_scale(k2_pos, 2.0)),
-                              vec3_add(vec3_scale(k3_pos, 2.0), k4_pos));
-
-    *velocity = vec3_add(vel0, vec3_scale(k_vel_sum, dt / 6.0));
-    *position = vec3_add(pos0, vec3_scale(k_pos_sum, dt / 6.0));
-}
-
-Vec3 evaluate_acceleration(Vec3 relative_pos, double body_mass, double parent_mass) {
-    Vec3 total_force = {0.0, 0.0, 0.0};
-
-    double distance = vec3_magnitude(relative_pos);
-    if (distance < 1.0) {
-        distance = 1.0;
-    }
-
-    double force_magnitude = G * body_mass * parent_mass / (distance * distance);
-    Vec3 direction = vec3_normalize(vec3_scale(relative_pos, -1.0));
-    total_force = vec3_scale(direction, force_magnitude);
-
-    return calculate_acceleration(total_force, body_mass);
-}
-
 Mat3 mat3_identity() {
     return {1.0, 0.0, 0.0,
             0.0, 1.0, 0.0,
@@ -172,3 +122,9 @@ Mat3 mat3_rotation_orbital(double omega, double i, double Omega) {
     Mat3 temp = mat3_multiply(Rx_i, Rz_omega);
     return mat3_multiply(Rz_Omega, temp);
 }
+
+bool compare_vec3(Vec3 a, Vec3 b, double tolerance) {
+    return fabs(a.x - b.x) <= tolerance &&
+           fabs(a.y - b.y) <= tolerance &&
+           fabs(a.z - b.z) <= tolerance;
+}
diff --git a/src/physics.h b/src/physics.h
index 5c8500c..5834890 100644
--- a/src/physics.h
+++ b/src/physics.h
@@ -35,16 +35,7 @@ Mat3 mat3_rotation_x(double angle);
 Mat3 mat3_rotation_z(double angle);
 Mat3 mat3_rotation_orbital(double omega, double i, double Omega);
 
-// Physics functions
-Vec3 calculate_acceleration(Vec3 force, double mass);
-
-// Physics integration functions
-// RK4 inferior to analytical propagation for orbit simulation
-// In our specific simulation (2-body with SOI patched conics):
-// Analytical: <1e-12 energy drift vs RK4: 2e-7 to 5e-3
-// See tests/test_hybrid_energy_conservation.cpp for comparison
-void rk4_step(Vec3* position, Vec3* velocity, double dt,
-              double body_mass, double parent_mass);
-Vec3 evaluate_acceleration(Vec3 relative_pos, double body_mass, double parent_mass);
+// Comparison utility
+bool compare_vec3(Vec3 a, Vec3 b, double tolerance);
 
 #endif
diff --git a/src/test_utilities.cpp b/src/test_utilities.cpp
index bbc7a7c..cac2ce6 100644
--- a/src/test_utilities.cpp
+++ b/src/test_utilities.cpp
@@ -45,12 +45,6 @@ OrbitalMetrics calculate_orbital_metrics(CelestialBody* body, CelestialBody* par
     return metrics;
 }
 
-bool compare_vec3(Vec3 a, Vec3 b, double tolerance) {
-    return fabs(a.x - b.x) <= tolerance &&
-           fabs(a.y - b.y) <= tolerance &&
-           fabs(a.z - b.z) <= tolerance;
-}
-
 OrbitTracker* create_orbit_tracker_with_min_time(int body_index, double min_time_seconds) {
     OrbitTracker* tracker = (OrbitTracker*)malloc(sizeof(OrbitTracker));
     tracker->body_index = body_index;
diff --git a/src/test_utilities.h b/src/test_utilities.h
index 70b3154..bea7414 100644
--- a/src/test_utilities.h
+++ b/src/test_utilities.h
@@ -62,6 +62,4 @@ void destroy_orbit_tracker(OrbitTracker* tracker);
 int dump_simulation_state(SimulationState* sim, const char* label,
                           char* buffer, int buffer_size);
 
-bool compare_vec3(Vec3 a, Vec3 b, double tolerance);
-
 #endif