def fuel_for_missions(interface):
# unpack data
config = interface.configs.cruise
analyses = interface.analyses
mission = interface.analyses.missions.fuel.mission
mission_payload = interface.analyses.missions.fuel.payload
# determine maximum range based in tow short_field
from SUAVE.Methods.Performance import size_mission_range_given_weights
# unpack
cruise_segment_tag = 'cruise'
weight_max = config.mass_properties.max_takeoff
weight_min = config.mass_properties.operating_empty + 0.10 * mission_payload # 10%
takeoff_weight_vec = np.linspace(weight_min,weight_max,3)
distance_vec = np.zeros_like(takeoff_weight_vec)
fuel_vec = np.zeros_like(takeoff_weight_vec)
# call function
distance_vec,fuel_vec = size_mission_range_given_weights(config,mission,cruise_segment_tag,mission_payload,takeoff_weight_vec)
# pack
results = Data()
results.tag = 'missions_fuel'
results.weights = takeoff_weight_vec
results.distances = distance_vec
results.fuels = fuel_vec
## print results
return results
