UnboundLocalError: local variable 'radius' referenced before assignment

[Gui-FernandesBR]

Describe the bug

Reported today on discord: thread ID: 1337930498739277898

MRT014 [LURA]
OP
— Today at 8:38 PM
We're using a creating a rocket and we're having an issue with the radius. The stability is also way off as well. I've attached the output as a txt file since there's a character limit. Any help would be much appreciated

config.py
sustainer_po_cd, sustainer_poff_cd, sustainer_cp = parse_rasaero_file(join(this_dir, "data", "sustainer.CSV"))
SUSTAINER_PARAMS = {
"radius": 0.057/2,
"mass": 1.687, # airframe mass
"inertia": (645548/(110**9), # x
229864458/(1109),# y
229883464/(1*109) # z
), # Just airframe
"coordinate_system_orientation": "nose_to_tail",
"center_of_mass_without_motor": 0.829,
"power_on_drag": sustainer_po_cd,
"power_off_drag": sustainer_poff_cd,
"center_of_pressure_source": sustainer_cp
}

sustainer.py
from lura_rockets.G2_DART.CDR import config
from lura_rockets.supersonic_rocket import SupersonicRocket

===== ROCKET =====

dart = SupersonicRocket(**config.SUSTAINER_PARAMS)

===== PARACHUTE =====

main_parachute = dart.add_parachute(**config.SUSTAINER_MAIN_PARACHUTE, sampling_rate=100)
drogue_parachute = dart.add_parachute(**config.SUSTAINER_DROGUE_PARACHUTE)

dart.all_info()

Running
sustainer.py
output

Expected behavior

MRT014 [LURA]
OP
— Today at 8:54 PM
Fixed this. Rockets are required to have atleast one aero surface otherwise the loop in
rocketpy/plots/rocket_plots.py
in the function
_draw_tubes
exits prematurely and therefore the return value
radius
has not been defined
Gui [RocketPy Team] — Today at 9:24 PM
We should allow the draw method to work properly even if no aerosurface is provided. Thanks for opening this question!

Additional context

Should be quite easy to solve the problem.