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ACAZ C 2 AIRCRAFT |
Version française |
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Description and
characteristics of the aircraft
(Images and texts of the origin plans of 1925)
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Main advantages of this
aircraft The aircraft ACAZ, typifies C2 - engine Hispano-Suiza type 51-12H in V gives 462 cv at 1800 tr/mn (normal speed) - is a two-seater biplane of completely metal fight including the covering of wings. 1) Remarkable performances thus weapon of fight allowing to compete with the best foreign types. 2) Total visibility obtained by the gap of wings and bights to both plans ; the pilot and the machine gunner are in a small nacelle dominating the fuselage. By these means the pilot can see above and below the superior wing and the visibility on the sides of the fuselage is strikingly increased with regard to the other devices. Furthermore, being in the same nacelle, the pilot and the machine gunner can communicate easily. 3) Big handiness, the masses being strictly grouped. Gone up extra fast. 4) Several systems protecting the life of the occupants are foreseen: a) Gas tank with lid largable ACAZ system. b) Fire extinguisher. c) Parachute for pilot and machine gunner ; easy evacuation because of wings and of nacelle. d) Stiff nacelle forming frame of protection in case of accidents. 5) Solid but simple metal construction allowing a mass stake without excessive equipment. The metal construction allows the stay the bad weather without damages for the device. 6) Simple and fast regulation foreseen for the cell and the empennages. 7) Conception ahead of the current programs thus type of current aircraft for a big number of years. In summary : a beautiful war weapon ; fast, solid, handy and very elegant being able to compete and even outstrip all the existing devices or under construction ; prototype nowadays. |
Characteristics |
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Scale 12,5 m Dihedral of the superior wing 4° Dihedral of the lower wing 0° Way of the landing gear 2m Section of the fuselage to the boss couples: 0,9 x 1,38 m Total length 8,25 m Maximum height 3,4 m Surface superior wings (including ailerons) 21,36 m ² Surface lower wings (including ailerons) 19,2 m ² Carrying surface 40,56 m ² Total surface of 4 ailerons 4,88 m ² Total surface of the elevator 2,84 m ² Total surface of the static shot 2,94 m ² Total surface of the plan(shot) of drift 0,58 m ² Total surface of the rudder 0,985 m ² |
Outstrip graft plans
1,60 m Depth of wings (superiors and subordinates) 1,86 m Gap of wings 750 m/m Slope of wings with regard to the axis of fuselage + 3° Slope of the engine with regard to the axis of fuselage 0° Centring: parasol. Axis of drive of the engine below the centre of gravity. Little taken away centres, Stability in any slopes guarantee by the essays in the tunnel. Profile of wing ACAZ N 2 - very fine speed wing, the centre of pressure of which varies little (Conclusion of the essays in the laboratory). Charge at m ² : 46,9 kgr Charge at CV : 4,11 kgr |
Estimate of the Weights Wings, hut, checkmates and shrouds of wings with all the horseshoes, the ailerons 300 kg Fuselage 105 kg Empennages, govern 35 kg Atterrisseur complete 65 kg Weight of fuel for 3 1/2 the hour of flight ; gasoline(essence) 380 kg, oils 25 kg Vacuous engine + helix (without water) 435 kg Radiator + water total 105 kg Live weight (Pilot, machine gunner, equipment, armament, developments, T.S.F, parachutes) 350 kg Commands, tanks, divers and unforeseen 100 kg Total weight: 1900 kg Performances found by the essay in the tunnel of the model of the plane By the Belgian aerodynamic laboratory Maximum speed on the ground with full load 225 kph Minimum speed on the ground with full load 86 kph Radius of action 790 km. Ceiling 7400 m. Speed in the ceiling 155 kph |
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Thanks to Yves Duwelz, to Jean Pierre Lauwers, to Didier Campion, to Rod Filan, to Jan den Das, to Jacques Willems, to Luc Wittemans and to Gérard Rooss for informations and documents relative to the history of ACAZ C2 which they sent me. |
C2 model exists in scale 1/72 at Omega Models
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RM
Contact :
rolharmo@orange.fr
Last Update,
January 2021