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The Aero Ae.02 marked the first all-Czech-designed biplane fighter in its history - only one flyable prototype was completed.
Detailing the development and operational history of the Aero Ae.02 Single-Seat Biplane Fighter Prototype. Entry last updated on 6/21/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com
The Ae.02 benefitted from experiences gained by the major air powers of World War 1. It utilized a streamlined fuselage and an upper and lower wing (unequal span) assembly braced by a simplified I-strut arrangement. The strut and wing arrangement created single bays to each side of the fuselage. Ailerons were featured along the upper wing members only and the wings themselves were fabric-covered wood appendages. Internally, duralumin alloy was used to make up the aircraft's load-bearing framework. The engine was held at a forward compartment in the traditional way and drove a two-bladed propeller unit at the nose. The undercarriage was fixed in flight and wheeled at the main leg members. The tail utilized a traditional single-finned arrangement.
Proposed armament became 2 x 7.7mm Vickers Machine Guns synchronized to fire through the spinning propeller blades. Beyond this there was no bomb-carrying capability built-in.
Dimensions amounted to a length of 17.10 feet, a wingspan of 27 feet and a height of 8.9 feet. Empty weight was 1,200lb against an MTOW of 1,910lb. Power was from a single Hispano-Suiza 8Ba V8 water-cooled inline piston engine generating 220 horsepower.
Josef Novak was at the controls of the prototype Ae.02 when it first went to the air in 1920. Beyond a 1st place finish in 1921 at the 1st International Flying Meeting (hosted by Czechoslovakia), the Ae.02 saw very little commercial success for it was not adopted for military service even by the local air force. Instead, attention turned to its evolved successor - the Ae.04 - leaving the sole Ae.02 prototype to the pages of aviation history.
Any available statistics for the Aero Ae.02 Single-Seat Biplane Fighter Prototype are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed Rating
This entry's maximum listed speed (140mph).
Graph average of 112.5 miles-per-hour.
Graph showcases the Aero Ae.02's operational range (on internal fuel) when compared to distances between major cities.