 This was achieved by placing a small tank ahead of the wing holding one third of the total oxidant (as well as the fuel in the shaped nose tank) and locating the main oxidant tank aft of the wing.Other large components were placed fore and aft of the wing.In the space below and above the wing centre section were located the air, fuel, oxidant and warm-air pipes, telemetering transmitter, instruments and batteries as well as the autopilot, timing clock, wiring terminal fuses and the connections by which the test vehicle was carried on the parent aircraft.