Northrop A-9

1972

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Northrop A-9

Under the designation Northrop YA-9A, the company built two prototypes of a single-seat close-support aircraft as the company's submission for the competitive development phase of the USAF's A-X close-support aircraft competition. A cantilever high-wing monoplane, powered by two 2722kg thrust Avco Lycoming ALF 502 turbofan engines, the first of the prototypes made its maiden flight on 30 May 1972. In competitive evaluation the YA-9A lost out to the YA-10A by Fairchild Republic.

Northrop A-9

Specification 
 CREW1
 ENGINE2 x Lycoming F-102-LD-100, 33.4kN
 WEIGHTS
  Take-off weight18160 kg40036 lb
  Empty weight10318 kg22747 lb
 DIMENSIONS
  Wingspan17.7 m58 ft 1 in
  Length16.3 m54 ft 6 in
  Height5.2 m17 ft 1 in
  Wing area54.9 m2590.94 sq ft
 PERFORMANCE
  Max. speed740 km/h460 mph
  Cruise speed740 km/h460 mph
  Range w/max.fuel4800 km2983 miles
 ARMAMENT1 x 30mm machine-guns, 7264kg of bombs and missiles


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