def mass_hpa_tail_boom(
        length_tail_boom,
        dynamic_pressure_at_manuever_speed,
        mean_tail_surface_area,
):
    """
    Finds the mass of a tail boom structure of a human powered aircraft (HPA), following Juan Cruz's correlations in
    http://journals.sfu.ca/ts/index.php/ts/article/viewFile/760/718
    Assumes a tubular tail boom of high modules (E > 228 GPa) graphite/epoxy
    :param length_tail_boom: length of the tail boom [m]. Calculated as distance from the wing 1/4 chord to the furthest tail surface.
    :param dynamic_pressure_at_manuever_speed: dynamic pressure at maneuvering speed [Pa]
    :param mean_tail_surface_area: mean of the areas of the tail surfaces (elevator, rudder)
    :return: mass of the tail boom [m]
    """
    l = length_tail_boom
    q = dynamic_pressure_at_manuever_speed
    area = mean_tail_surface_area
    w_tb = (l * 1.14e-1 + l ** 2 * 1.96e-2) * (1 + ((q * area) / 78.5 - 1) / 2)

    return w_tb