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Rockwell Ranger 2000

Military Aircraft

The Rockwell Ranger 2000 was a two-seat jet trainer that Rockwell International proposed for the United States Joint Primary Aircraft Training System, with help from the German firm Rhein-Flugzeugbau. It was a single-engine, low-wing monoplane with tandem seating, retractable tricycle landing gear and a rear fuselage Pratt and Whitney Canada JT15D-5C turbofan fed by intakes above the wing roots, and its design drew on the RFB Fantrainer. The prototypes were built in Germany, the first flying on 15 January 1993 at Manching. The second prototype was lost in an accident that July, and the type lost the competition to a variant of the Pilatus PC-9, later the T-6 Texan II. One survivor is displayed at the Tulsa Air and Space Museum.

Facts
Year
1993 1
Engine Class
Jet 1
Status
Surviving 1
Top Speed (km/h)
630 1
Engine
Pratt & Whitney Canada JT15D-5C 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Rockwell Ranger 2000 (Wikipedia)

Of Make

Source Rockwell Ranger 2000 (Wikipedia)
Sources
1. Rockwell Ranger 2000 (Wikipedia)
  • Design and development, first flight
    The aircraft first flew on 15 January 1993 at Manching in Germany.
  • Lead
    was a jet trainer candidate for the United States Joint Primary Aircraft Training System
  • Design and development, powerplant
    The Ranger 2000 was powered by a Pratt & Whitney Canada JT15D-5C turbofan mounted in the rear fuselage
  • Specifications, performance
    Maximum speed: 392 mph (630 km/h, 341 kn)
  • Aircraft on display
    One of the Ranger 2000s is displayed at the Tulsa Air and Space Museum.
  • Lead, manufacturer
    proposed by Rockwell International with assistance from Rhein-Flugzeugbau GmbH (RFB) in Germany
  • Exemplifies: Aviation, Lead, mode
    a jet trainer candidate
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