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The cabin width was 28 in (71 cm). The acceptable power range was 28 to 42 hp (21 to 31 kW) and the standard engine used was the 40 hp (30 kW) Hirth 2702 two-stroke powerplant. [1] The Freedom 40 had a typical empty weight of 330 lb (150 kg) and a gross weight of 600 lb (270 kg), giving a useful load of 270 lb (120 kg).
The aircraft is designed to cruise at 45,000 ft (14,000 m) at speeds up to 435 knots (Mach 0.76) and fly as far as 4170 km - while consuming about 40% less fuel than conventionally built planes - using two GE Honda HF120 engines.
Since approximately 2006, the company has been involved in the development of two very light jets, the Spectrum S-33 "Independence" and the S-40 "Freedom", which are to be constructed making extensive use of composite materials. The twin-engined single pilot aircraft are supposed to carry between five and nine passengers over distances between ...
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This page was last edited on 19 December 2013, at 01:40 (UTC).; Text is available under the
The Northrop F-5 is a family of supersonic light fighter aircraft initially designed as a privately funded project in the late 1950s by Northrop Corporation.There are two main models: the original F-5A and F-5B Freedom Fighter variants, and the extensively updated F-5E and F-5F Tiger II variants.
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