test_flight_liftoff_mass Namespace Reference

Functions
	_fly (liftoff=None)
	as_configured ()
	test_the_budget_is_rocketpys_own_total (as_configured)
	test_a_weighed_vehicle_lifts_off_at_its_weight_and_flies_lower (as_configured)
	test_a_liftoff_mass_lighter_than_the_motor_is_refused (as_configured)
	_fly_with (liftoff=None, gas=None)
	test_the_drawings_ullage_gas_flies_with_the_vehicle (as_configured)

Variables
float	LB = 0.45359237

Detailed Description

The vehicle flies at the liftoff mass it was weighed at.

Judged by RocketPy's own mass bookkeeping (``rocket.total_mass(0)``), not by the arithmetic that
sets the airframe: the airframe is set from the booked motor, propellants and gases, and RocketPy
sums its tanks and gases independently.

Function Documentation

_fly()

test_flight_liftoff_mass._fly ( liftoff = None )

protected

Definition at line 22 of file test_flight_liftoff_mass.py.

Referenced by as_configured(), test_a_liftoff_mass_lighter_than_the_motor_is_refused(), and test_a_weighed_vehicle_lifts_off_at_its_weight_and_flies_lower().

_fly_with()

test_flight_liftoff_mass._fly_with ( liftoff = None, gas = None )

protected

Definition at line 62 of file test_flight_liftoff_mass.py.

Referenced by test_the_drawings_ullage_gas_flies_with_the_vehicle().

as_configured()

test_flight_liftoff_mass.as_configured

(

)

Definition at line 34 of file test_flight_liftoff_mass.py.

References _fly().

test_a_liftoff_mass_lighter_than_the_motor_is_refused()

test_flight_liftoff_mass.test_a_liftoff_mass_lighter_than_the_motor_is_refused

(

as_configured

)

Definition at line 57 of file test_flight_liftoff_mass.py.

References _fly().

test_a_weighed_vehicle_lifts_off_at_its_weight_and_flies_lower()

test_flight_liftoff_mass.test_a_weighed_vehicle_lifts_off_at_its_weight_and_flies_lower

(

as_configured

)

Definition at line 44 of file test_flight_liftoff_mass.py.

References _fly().

test_the_budget_is_rocketpys_own_total()

test_flight_liftoff_mass.test_the_budget_is_rocketpys_own_total

(

as_configured

)

Definition at line 38 of file test_flight_liftoff_mass.py.

test_the_drawings_ullage_gas_flies_with_the_vehicle()

test_flight_liftoff_mass.test_the_drawings_ullage_gas_flies_with_the_vehicle

(

as_configured

)

Definition at line 73 of file test_flight_liftoff_mass.py.

References _fly_with().

Variable Documentation

LB

float test_flight_liftoff_mass.LB = 0.45359237

Definition at line 19 of file test_flight_liftoff_mass.py.