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The original Pulsar was a hatchback to be sold exclusively at a different Nissan Japan dealership network called Nissan Cherry Store as a larger five-door hatchback alternative to the Nissan Cherry. Although Pulsar models were front-wheel drive from introduction, Nissan did offer four-wheel drive as an option on select models internationally.
Rotax 582 pusher installation on a Quad City Challenger II: Type Piston aero-engine: National origin: Austria Manufacturer Rotax: Major applications: Quad City Challenger Blue Yonder Merlin: Status Production to be completed by end of 2021 [1] Produced 1989-2021 [1] [2] Number built: more than 30,000 (July 2021) [1]
The Aero Designs Pulsar is an American two-seat, low wing, ultralight and homebuilt aircraft that was designed by Mark Brown and first produced by Aero Designs of San Antonio, Texas, introduced in 1985. When it was available the Pulsar was supplied as a ready-to-fly aircraft and as a kitplane for amateur construction. [1] [2]
The SR engine is a series of 1.6 L (1,596 cc), 1.8 L (1,838 cc) or 2.0 L (1,998 cc) straight-four, four-stroke gasoline engines manufactured by Nissan.It has an aluminium head and block with steel sleeves and has a DOHC 4-valve design, with variable valve timing on select models.
Rotax 912ULS 100 hp (75 kW) installation in a Blue Yonder Merlin EZ Pusher engine installation of two Rotax 912ULSs in a Lockwood Aircam Rotax 912ULS with tuned exhaust in a Dyn'Aéro MCR01 with 3-blade hydraulic CSU propeller. The Rotax 912 is a horizontally-opposed four-cylinder, naturally-aspirated, four-stroke aircraft engine with a ...
2007 Toyota Yaris hatchback owner's manual 1919 Ford Motor Company car and truck operating manual. An owner's manual (also called an instruction manual or a user guide) is an instructional book or booklet that is supplied with almost all technologically advanced consumer products such as vehicles, home appliances and computer peripherals.
A T56 on a mobile test unit at MCAS Futenma, 1982 T56-A-1 (Series I) A 1,600 lb weight (730 kg) engine delivering 3,460 shp (2,580 kW) and 725 lbf (329 kgf; 3.22 kN) residual jet thrust, which is equal to 3,750 equivalent shp (2,800 kW); single-shaft 14-stage axial flow compressor, cannular combustion chamber with 6-cylindrical through-flow combustion liners, 4-stage axial flow turbine; 13,800 ...
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