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thesis/julia/sft.jl
rconnorjohnstone 7296df65bc Began!
2021-05-17 21:32:25 -06:00

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Julia

"""
Maximum ΔV that a spacecraft can impulse for a given single time step
"""
function max_ΔV(duty_cycle::Float64,
num_thrusters::Int,
max_thrust::Float64,
tf::Float64,
t0::Float64,
mass::Float64)
return duty_cycle*num_thrusters*max_thrust*(tf-t0)/mass
end