The paper presents technologies of reducing the technological environmental impact of man-made space launch vehicles (SLV) based on controlled descent and trajectories of deorbiting the spent stages. burning of the separated nose fairing halves and tail section in the atmosphere. Controlled descent of a spent stage is accomplished due to the installation of an active on-board recovery... https://www.roneverhart.com/Whirlwind-Direct-2-Direct-Box-p14308/