ENH: burnout time changes. Breaking changes

README.md

@@ -206,7 +206,7 @@ A sample Motor object can be created by the following code:
 ```python
 Pro75M1670 = SolidMotor(
     thrustSource="../data/motors/Cesaroni_M1670.eng",
-    burnOut=3.9,
+    burn_time=3.9,
     grainNumber=5,
     grainSeparation=5/1000,
     grainDensity=1815,

docs/development/rocketpy_as_developer.rst

@@ -125,7 +125,7 @@ The motor class contains information about the thrust curve and uses some geomet
 
     Pro75M1670 = SolidMotor(
         thrustSource="../data/motors/Cesaroni_M1670.eng", #copy here the path to the thrust source file
-        burnOut=3.9,
+        burn_time=3.9,
         grainNumber=5,
         grainSeparation=5 / 1000,
         grainDensity=1815,

docs/matlab/Getting_Started.m

@@ -80,7 +80,7 @@
 
 Pro75M1670 = rocketpy.SolidMotor(pyargs( ...
     'thrustSource', "../../data/motors/Cesaroni_M1670.eng", ...
-    'burnOut', 3.9, ...
+    'burn_time', 3.9, ...
     'grainsCenterOfMassPosition', -0.85704, ...
     'grainNumber', int32(5), ...
     'grainSeparation', 5 / 1000, ...

docs/notebooks/SEBLM.ipynb

@@ -29,6 +29,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -64,6 +65,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -84,6 +86,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -116,6 +119,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -148,6 +152,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -190,6 +195,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -204,7 +210,7 @@
    "source": [
     "SEBLM = LiquidMotor(\n",
     "    thrustSource=\"../../data/SEBLM/test124_Thrust_Curve.csv\",\n",
-    "    burnOut=20.0,\n",
+    "    burn_time=20.0,\n",
     "    nozzleRadius=0.069/2,\n",
     "    nozzlePosition=-1.364,\n",
     "    coordinateSystemOrientation=\"nozzleToCombustionChamber\",\n",
@@ -259,6 +265,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -356,6 +363,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": [
@@ -370,6 +378,7 @@
    ]
   },
   {
+   "attachments": {},
    "cell_type": "markdown",
    "metadata": {},
    "source": []

docs/notebooks/compare_flights_usage.ipynb

@@ -74,7 +74,7 @@
     "\n",
     "Pro75M1670 = SolidMotor(\n",
     "    thrustSource=\"../../data/motors/Cesaroni_M1670.eng\",\n",
-    "    burnOut=3.9,\n",
+    "    burn_time=3.9,\n",
     "    grainsCenterOfMassPosition=-0.85704,\n",
     "    grainNumber=5,\n",
     "    grainSeparation=5 / 1000,\n",