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The Harrier GR.9 is an avionics and weapons upgrade of the standard GR.7. [1] GR.9A The Harrier GR.9A is an avionics and weapons upgrade of the uprated engined GR.7As. All GR.9s are capable of accepting the Mk 107 Pegasus engine to become GR.9As. [1] T.10 The Harrier T.10 is the original two seat training variant of the
RAF Harrier GR9 in flight, 2010. The Harrier II is an extensively modified version of the first generation Harrier GR1/GR3 series. The original aluminium alloy fuselage was replaced with one made extensively of composites, providing significant weight reduction and increased payload or range.
The Harrier II retains the tandem landing gear layout of the first-generation Harriers, although each outrigger landing gear leg was moved from the wingtip to mid-span for a tighter turning radius when taxiing. [69] The engine intakes are larger than those of the first-generation Harrier and have a revised inlet.
The use of "G" to denote twin cam engines was decided on in 1971, with the renaming of the 10R into 8R-G. Before that, twin cams had received separate numerical codes. [1] In 1987, Toyota began assigning dual letter engine codes to some of the "engine family" categories in some engine lines, particularly six-cylinder models.
Compared with the outgoing model, the width and the wheelbase is up by 20 mm (0.8 in) and 30 mm (1.2 in) respectively, while the height has been cut by 30 mm (1.2 in). Unlike the previous model, the turbocharged engine option is not available in this generation. It is available in S, G and Z grade levels in Japan.
This is an alphabetical list of aircraft engines by manufacturer ... Bristol BE53 Pegasus (later, BS53 the Harrier engine ... Initial development model using Boeing ...
GSU Platform (2GR engine) 2003–2009 Toyota Harrier; 2007–present Toyota Highlander; 2006–2008 Lexus RX350; ... Models Engines AN10, AN20, AN30. Toyota Hilux ...
Rolls-Royce Bristol Pegasus, engine of the vertical takeoff Harrier, in the Bristol Industrial Museum, England. Pegasus 1 (BE53-2) The two prototype engines were demonstrator engines which developed about 9,000 lbf (40 kN) on the test bed. Neither engine was installed in a P.1127. Pegasus 2 (BE53-3) Used in the initial P.1127s, 11,500 lbf (51 kN)