“…For this, we use the method of Hill et al (1994) [1], viewing the aircraft cabin as a reverberant microwave cavity in which only four loss mechanisms are possible: (1) loss due to escape from the cavity, (2) loss due to absorption by lossy media, (3) loss due to finite wall conductivity, and (4) loss due to intercept by other antennas. We assume that the loss due to mechanisms (3) and (4) is insignificant compared to the first two mechanisms, and we further assume that transmission through windows is the dominant contribution to (1). Under these assumptions, the ratio of power escaping the cabin (through windows) to total power transmit is L w ≈ Q 2 /(Q 2 + Q 3 ) where Q 2 and Q 3 are "quality factors" associated with absorption and escape loss, respectively, obtained from expressions in [1].…”