test_timeseries_fill_levels._Runner Class Reference

Public Member Functions
	__init__ (self, lox_load, fuel_load, mdot_O=1.8755, mdot_F=1.2451)
	evaluate_arrays (self, P_O, P_F)

Public Attributes
	config
tuple	m = (mdot_O, mdot_F)

Detailed Description

Definition at line 19 of file test_timeseries_fill_levels.py.

Constructor & Destructor Documentation

__init__()

test_timeseries_fill_levels._Runner.__init__	(		self,
			lox_load,
			fuel_load,
			mdot_O = 1.8755,
			mdot_F = 1.2451 )

Definition at line 20 of file test_timeseries_fill_levels.py.

Member Function Documentation

evaluate_arrays()

test_timeseries_fill_levels._Runner.evaluate_arrays	(		self,
			P_O,
			P_F )

Definition at line 27 of file test_timeseries_fill_levels.py.

References detail::exception.m, engine.layerx.flight.InlineAscent.m, engine.pipeline.config_schemas.SMDConfig.m, m, and time.m.

Member Data Documentation

config

test_timeseries_fill_levels._Runner.config

Initial value:

=  types.SimpleNamespace(
            ablative_cooling=None, press_tank=None,
            lox_tank=types.SimpleNamespace(mass=lox_load), fuel_tank=types.SimpleNamespace(mass=fuel_load),
        )

Definition at line 21 of file test_timeseries_fill_levels.py.

m

test_timeseries_fill_levels._Runner.m = (mdot_O, mdot_F)

Definition at line 25 of file test_timeseries_fill_levels.py.

Referenced by evaluate_arrays().

---

The documentation for this class was generated from the following file:

• EngineDesign/tests/test_timeseries_fill_levels.py