The 1913 Schwade 2-seater biplane was designed and built by Schwade in Germany
Schwade 1913 biplane
Era
Schmitt Type 7
The 1913 Schmitt Type 7 biplane was designed and built by Paul Schmitt in France.
In 1914 this plane broke 43 world records.
Span: upper 57’5″ lower 44’3″
Weight gross: 3300 lbs
Speed: 27-78 mph
Incident variation: between o° and 12°.
Rumpler 1913 monoplane
The 1913 Rumpler monoplane was designed and built by Rumpler Company in Germany
Vuia, Trajan
Ozone Spyder
The 2025 Spyder 4 is the lightweight version of the Roadster 4. It uses a carefully selected blend of lightweight fabrics for the main surfaces and ribs, along with an optimised internal construction, reducing both sail weight and packing volume. Using lightweight fabric in a paramotor wing has positive effects all around, the main advantages are faster inflation for easier launches, improved handling, a more agile and responsive feel, as well as enhanced passive safety thanks to reduced sail inertia.
Ozone Vibe
To be released early 2026 is the Vibe GT. The original Vibe was launched back in 2003 and was a huge success among progressing and experienced pilots alike needing the performance glider they trust in all conditions. The Vibe GT with its semi-light construction takes its name from the original, targeting the same pilots, the same pleasure to fly, in the most modern and efficient construction.
The Vibe GT is a 5.4 AR glider, EN-B certified, positioned between the Buzz/Geo and the Rush/Swift, offered in a semi-light GT package.
Ozone Alta
The 2025 Alta GT is the Alta re-labeled inside the semi-light GT Range. It offers new colours and a new XXS version certified from 50 to 65kg with a 20m² flat area. It packs up the best level of performance achievable in the category while retaining the ease of use found in the EN-A class. It combines the lightness needed for hike and fly or traveling, and the durability expected by novice pilots.
Ozone Wisp
The 2025 second generation of the Wisp delivers the lightest double-surface tandem in existence at 4.15kg. Designed for Alpine adventures and travel, this all new wing is incredibly easy to use which suits it perfectly for improvised launches and tricky conditions. With performance in line with intermediate category wings, the EN-B Wisp 2 will take you and your partner to distances never flown by ultralight tandems.
Pratt & Whitney PW1120
Development of the PW1120 to Israeli Air Force (IDF/AF) specifications began in June 1980. It retained the F100 digital electronic control system, along with the F100 main module transmission fuel pump forward channels, with only minor modifications. Unique PW1120 components include a wide-chord low-pressure (LP) compressor, a single-stage uncooled low-pressure (LP) turbine with a simplified single-flow booster, and a lightweight convergent/divergent nozzle. Full-scale testing began in June 1982, and the PW1120’s flight permit testing began in August 1984. The PW1120 had a 70% similarity to the F100, so the IDF/AF would not need a dedicated facility for spare parts. It was to be built under license by Bet-Shemesh Engines Limited in Israel.
IAI installed a PW1120 on the starboard bed of an F-4E-32-MC of the IDF/AF (Number 334/66-0327) to explore the airframe/engine combination for an upgrade program for the F-4E known as the Kurnass 2000 (“Heavy Hammer”) or to serve as an engine testbed for the Super Phantom and Lavi. The engine was more powerful and more fuel-efficient than the General Electric J79-GE-17 turbojet normally fitted to the F-4E.
Structural changes included modified air intake ducts, new powerplant ports, new or modified powerplant bay doors, integrated drive generators, and a new fuselage-mounted gearbox with an autothrottle system. It also included a modified bleed management and air conditioning ducting system, modified fuel and hydraulic systems, and a powerplant control/airframe interface. It first flew on 30 July 1986.
Two PW1120 power plants were installed in the same F-4E and first flew on 24 April 1987. This proved very successful, allowing the Kurnass 2000 to exceed Mach 1 without afterburners and have a combat thrust-to-weight ratio of 1.04. This improved the sustained turn ratio by 15 percent, the climb rate by 36 percent, mid-level acceleration by 27 percent, and the low-level speed from 1,046 km/h to 1,120 km/h (654 to 700 mph) with 18 bombs (or 565 kn to 605 kn). It was demonstrated at the 1987 Paris Air Show.
Avro 538
The Avro 538 was a considerably modified development of the basic Avro 531 design with equal-span wings, normal wing strutting and a larger upper wing/fuselage gap.
Intended as a racing aircraft, the 538 was never used as such because of a defective spar. Powered by a 150 hp / 112 kW Bentley B.R.2, it was used by Avro Transport Co as a communication aircraft from May 1919 until September 1920.
Engine: 150 hp / 112 kW Bentley B.R.2
Wingspan: 8.53 m / 28 ft 0 in
Height: 2.59 m / 8 ft 6 in
Wing area: 19.51 sq.m / 210.0 sq ft
Empty weight: 442 kg / 975 lb
Take-off weight: 635 kg / 15400 lb
Range: 320 mi / 515 km
All Aero 