• Soviet engineers opted for a midair launch scheme for Spiral. Known as "50 / 50", the idea was that the spaceplane and a liquid fuel booster stage would be launched at high altitude from the back of a custom-built
hypersonic jet. The mothership was to have been built by the
Tupolev Design Bureau (OKB-156) and utilize many of the same technologies developed for the
Tu-144 supersonic transport and the
Sukhoi T-4 Mach 3 bomber. It was never built. • Spiral was a conventional
delta wing that featured innovative variable-
dihedral wings. During launch and reentry, these were folded upward at 60 degrees. After dropping to subsonic speeds post-reentry, the pilot lowered the wings into the horizontal position, giving the spaceplane better re-entry and flight characteristics. • Spiral was built to allow for a powered landing and go-around maneuver in case of a missed landing approach. An air intake for a single Kolesov turbojet was mounted beneath the central vertical stabilizer. This was protected during launch and re-entry by a clamshell door which opened at subsonic speeds. • Spiral was to have been protected by what Soviet engineers termed "scale-plate armour":
niobium alloy VN5AP and
molybdenum disilicide plated steel plates mounted on articulated ceramic bearings to allow for
thermal expansion during reentry. Several BOR (Russian acronym for Unpiloted Orbital Rocketplane) craft were flown to test this concept. • In the event of a booster explosion or in-flight emergency, the
crew compartment of Spiral was designed to separate from the rest of the vehicle and parachute to earth like a conventional ballistic capsule; this could be done at any point in the flight. • Spiral was intended to carry only its pilot. • Spiral was designed to land on skids, which deployed from a set of doors on the sides of the fuselage just above and ahead of the wings. ==BOR reentry test vehicles==