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only_radial_burn on hybrid corrected
only_radial_burn argument order corrected
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rocketpy/motors/hybrid_motor.py

Lines changed: 2 additions & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -215,8 +215,8 @@ def __init__( # pylint: disable=too-many-arguments
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reshape_thrust_curve=False,
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interpolation_method="linear",
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coordinate_system_orientation="nozzle_to_combustion_chamber",
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only_radial_burn=True,
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reference_pressure=None,
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only_radial_burn=True,
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):
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"""Initialize Motor class, process thrust curve and geometrical
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parameters and store results.
@@ -364,8 +364,8 @@ class Function. Thrust units are Newtons.
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reshape_thrust_curve,
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interpolation_method,
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coordinate_system_orientation,
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only_radial_burn,
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reference_pressure,
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only_radial_burn,
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)
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self.positioned_tanks = self.liquid.positioned_tanks

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