Search results
Results From The WOW.Com Content Network
Data from AgustaWestland, Airbus Helicopters, The International Directory of Military Aircraft, 2002/2003 General characteristics Crew: 2 flight crew + loadmaster / sensor operator Capacity: 20 seated troops; or 12 medevac stretchers; or 2 NATO pallets; or 4,200 kg (9,259 lb) external slung load Length: 16.13 m (52 ft 11 in) Empty weight: 6,400 kg (14,110 lb) Max takeoff weight: 10,600 kg ...
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 only as published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.
The NHIndustries NH90 is a medium-sized, twin-engine, multi-role military helicopter developed in response to NATO requirements calling for a battlefield helicopter which would also be capable of being operated in naval environments. Both development and manufacture of the rotorcraft has been principally handled by NHIndustries, a collaborative ...
Finnish NH90 Swedish NH90 Danish AW101. Nordic Standard Helicopter Program (NSHP) was an international helicopter procurement program in the late 1990s and early 2000s to choose a standard helicopter for Norway, Sweden, Finland, and initially Denmark. In 1999, the four countries issued a requirement for a helicopter in the 9-15 ton range, which ...
NHI NH90, medium-sized, twin-engine, multi-role military helicopter manufactured by NHIndustries. Topics referred to by the same term This disambiguation page lists articles associated with the same title formed as a letter–number combination.
For now, you can take a crack at the hardest math problems known to man, woman, and machine. For more puzzles and brainteasers, check out Puzzmo . More from Popular Mechanics :
[10] In 1987, Canada selected the EH101 to replace its Sea Kings in the anti-submarine warfare and search and rescue roles. The EH101's third engine and increased range compared favourably with rival aircraft, such as the Sikorsky Seahawk. The range and de-icing capability were also seen as vital for North Atlantic operations. [11]
The engine was designed for the Hughes AH-64 Apache and Sikorsky UH-60 Blackhawk, competing with the General Electric T700 and the Pratt & Whitney Canada PW100.The partners shared the £100 million development costs equally, Rolls-Royce made the turbines, the combustor, and the inlet particle separator while Turbomeca produced the axial-centrifugal compressor and intake.