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2 GENERAL ELECTRIC 385 ENGINES ENGINE INTAKES. STANDARD FUEL CAPACITY 4,200 LB. JETFLAP PITCH AND ROLL CONTROL AS IN PRESENT AYROCAR (6 FT, FAN DRIVEN BY PARTIAL ENTRY TIP TURBINE EXHAUSTING UPWARDS ‘CARGO CAPACITY 100.0 CU. FT. ACCESSORIES BAYS ENGINES EXHAUST RETRACTABLE TREARWARDS EXTERNALLY FOCUSSING TYPE HOVERING taMpine Pans ACCESSORIES BAYS. ENGINES EXHAUST RETRACTABLE TREARWARDS EXTERNALLY FOCUSSING TYPE HOVERING [ANON PADS ‘CONTROL AND STABILIZER SYSTEM SIMIEAR TO AVROCAR FRONT COCKPIT FOR FAN INLET FAIRING ‘CENTRAL JET FOR GROUND CUSHION STABILIZATION — AND IMPROVED YTO THRUST EFFICIENCY HEIGHT 15 A. GROUND LINE ‘OVERALL LENGTH 20 FT. GROSS WT. FOR VIOL 9,700 LB, 79 Above: A test flight of the second VZ-9AV Avrocar at Malton in late 1958. Avro Canada Right: Advanced Mk 2 Avrocars. USAF Below left: Advanced Mk 2 Winged Avrocar. USAF Below right: Advanced Mk 2 Avrocar. USAF FIG 9 AVROCAR DEVELOPMENT FIG 10 AVROCAR DEVELOPMENT VERSION WITH WING EXTENSIONS Canada’s Cold War Saucers