Your Task

Write a function called EstimateLaunchCost that takes the following inputs $($in order$)$:

$-$ rocket$\_$weight $($in kg$)$: The rocket's base weight. This doees not include the payload.

$-$ fuel$\_$type: A string specifying the fuel type $("$Standard$"$ or "High$-$Efficiency"$).$ String comparisons are very picky; an extra space, a small typo, or a capital letter can cause your string comparison to fail. Please use the strings provided in the function template.

$-$ distance $($in km$)$: Total mission distance.

$-$ num$\_$stages: The number of rocket stages involved in the launch.

$-$ payload$\_$weight $($in kg$)$: The weight of the payload carried by the rocket.

The function should output two values:

$1.$ Total Launch Cost $($first output$)$: The total estimated cost of the rocket launch.

$2.$ Cost per Kilometer $($second output$)$: The average cost per kilometer traveled.

Use the following information to write your EstimateLaunchCost function.

$1.$ Base Cost per $\backslash (100\backslash$mathrm$\{$~km$\}$: $\backslash )$

$-$ For distances less than $200$ km $,$ the base cost is $\backslash (\backslash$$ $1,200\backslash )$ per $100$ km $.$

$-$ For distances greater than or equal to $200$ km $,$ the base cost is $\backslash (\backslash$$ $800\backslash )$ per $100$ km $.$

$2.$ Weight Surcharge:

$-$ If the rocket weight exceeds $\backslash (1,000\backslash$mathrm$\{$~kg$\}\backslash ),$ an additional surcharge of $\backslash (\backslash$$ $5,000\backslash )$ is added.

$3.$ Stage Cost:

$-$ Each rocket stage adds $\backslash (\backslash$$ $5,000\backslash )$ to the total cost.

$4.$ Payload Cost:

$-$ The cost of transporting the payload is $\backslash (\backslash$$ $500\backslash )$ per kilogram.

$5.$ Fuel Consumption:

$-$ Standard Fuel: Fuel cost of $\backslash (\backslash$$ $150\backslash )$ per km$.$

$-$ High$-$Efficiency Fuel: Fuel cost of $\backslash (\backslash$$ $120\backslash )$ per km$.$

The "default values" mentioned in the tests for this problem are:

$-$ rocket$\_$weight $\backslash (=1200\backslash$mathrm$\{$~kg$\}\backslash )$

$-$ payload$\_$weight $\backslash (=300\backslash$mathrm$\{$~kg$\}\backslash )$

$-$ distance $\backslash (=250\backslash$mathrm$\{$~km$\}\backslash )$

$-$ num$\_$stages $=2$