THE LOCKHEED MACH 3 AIRLINER THAT NEVER WAS скачать в хорошем качестве

THE LOCKHEED MACH 3 AIRLINER THAT NEVER WAS

The Lockheed L-2000 was Lockheed Corporation's entry in a government-funded competition to build the United States' first supersonic airliner in the 1960s. The L-2000 lost the contract to the Boeing 2707, but that competing design was ultimately canceled for political, environmental and economic reasons. In 1961, President John F. Kennedy committed the government to subsidizing 75% of the development of a commercial airliner to compete with the Anglo-French Concorde then under development. The director of the Federal Aviation Administration (FAA), Najeeb Halaby, elected to improve upon the Concorde's design rather than compete head-to-head with it. The SST, which might have represented a significant advance over the Concorde, was intended to carry 250 passengers (a large number at the time), fly at Mach 2.7-3.0, and have a range of 4,000 nmi (7,400 km).The program was launched on 5 June 1963, and the FAA estimated that by 1990 there would be a market for 500 SSTs. Boeing, Lockheed and North American officially responded. North American's design was soon rejected, but the Boeing and Lockheed designs were selected for further study. Specifications (L-2000-7A) General characteristics Capacity: 273 passengers Length: 273 ft 2 in (83.26 m) Wingspan: 116 ft (35.36 m) Height: () Wing area: 9,424 ft² (875 m²) Empty weight: 238,000 lb (107,900 kg) Max takeoff weight: 590,000 lb (276,600 kg) Powerplant: 4× GE4/J5M or Pratt & Whitney JTF17A-21L Performance Cruise speed: Mach 3.0 Range: 4,000 nmi (7,400 km) Service ceiling: 76,500 ft (23,317 km)