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lines changed Original file line number Diff line number Diff line change @@ -433,12 +433,13 @@ def bella_lui_point_mass_rocket(bella_lui_point_mass_motor):
433433def acceptance_point_mass_motor ():
434434 """Create a realistic point mass motor for acceptance testing.
435435
436- This is an alias for bella_lui_point_mass_motor to maintain compatibility.
436+ Uses the same Bella Lui rocket parameters (K828FJ motor) to provide
437+ a consistent baseline for all acceptance tests.
437438
438439 Returns
439440 -------
440441 rocketpy.PointMassMotor
441- A point mass motor with realistic thrust and mass properties .
442+ A point mass motor with Bella Lui rocket parameters .
442443 """
443444 return PointMassMotor (
444445 thrust_source = "data/motors/aerotech/AeroTech_K828FJ.eng" ,
@@ -452,7 +453,8 @@ def acceptance_point_mass_motor():
452453def acceptance_point_mass_rocket (acceptance_point_mass_motor ):
453454 """Create a realistic point mass rocket for acceptance testing.
454455
455- This is an alias for bella_lui_point_mass_rocket to maintain compatibility.
456+ Uses the same Bella Lui rocket parameters to provide a consistent
457+ baseline for all acceptance tests.
456458
457459 Parameters
458460 ----------
@@ -462,7 +464,7 @@ def acceptance_point_mass_rocket(acceptance_point_mass_motor):
462464 Returns
463465 -------
464466 rocketpy.PointMassRocket
465- A point mass rocket with realistic dimensions and properties .
467+ A point mass rocket with Bella Lui rocket parameters .
466468 """
467469 rocket = PointMassRocket (
468470 radius = 0.156 ,
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