Lockheed U-2R (TR-1A)
History reference (Taken from airwar.ru)
The TR-1A variant, which Lockheed built 28 units at the plant in Palmdale in 1979-1988, arose as a modification of the U-2R with significant changes in reconnaissance equipment, the installation of a new AN / UPO-X side-looking radar with synthesized image reproduction and modern means of electronic warfare. Initially, the TR-1A aircraft was planned to be used in the European theater of operations with the introduction of the PLSS (Precision Location Strike System) against targets in the territory of the Warsaw Pact countries.
Controls
Group 1 - open canopy
Group 3 - airbrakes
Group 4 - launch second engine
Group 7 - disconnect chassis
Cockpit controls
Big green ON button - retract landing gear
Switches under the ON button:
Red - group 1
Yellow - group 4
White - group 3
Big yellow button on the left side - group 7
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Specifications
Spotlights
- BoredGuy 2.6 years ago
General Characteristics
- Created On Android
- Wingspan 96.8ft (29.5m)
- Length 60.5ft (18.4m)
- Height 19.6ft (6.0m)
- Empty Weight 11,333lbs (5,140kg)
- Loaded Weight 24,623lbs (11,168kg)
Performance
- Power/Weight Ratio 1.985
- Wing Loading 26.1lbs/ft2 (127.5kg/m2)
- Wing Area 943.2ft2 (87.6m2)
- Drag Points 6976
Parts
- Number of Parts 191
- Control Surfaces 5
- Performance Cost 799