Editor -- pointing to
http://www.globalaircraft.org/planes/tu-22_blinder.pl
Format:
HTML
|
Text Only
Word wrap:
Off
|
On
<!--BEGIN SPECIFICATIONS--> Tu-22 Blinder Specifications Primary Function: Missile carrier / recce. platform Contractor: Tupolev Crew: N/A Unit Cost: N/A Powerplant two 16000-kg (35,273-lb) afterburning thrust Koliesov VD-7M turbojets Dimensions Length: 132 ft 11.7 in (40.53 m) Wingspan: 77 ft 11 in (23.75 m) Height: 35 ft 0 in (10.67 m) Weights Empty: 88,185 lb (40,000 kg) Maximum Takeoff: 185,188 lb (84,000 kg) Performance Speed: 924 mph (802 kt) Ceiling: 60,040 ft (18300 m) -- Blinder-A Range: 1,926 miles (3100 km) Armament one 23-mm NR-23 cannon in radar-controlled tail turret, plus one AS-4 'Kitchen' stand-off missile recessed into the weapons bay <!--END SPECIFICATIONS--> <!--BEGIN ACHIEVEMENTS--> Tu-22 Blinder Achievements The Tu-22 was Russia's first successful attempt at fielding a supersonic bomber. <!--END ACHIEVEMENTS--> <!--BEGIN FEATURES--> <!-- Tu-22 Blinder Features --> <!--END FEATURES--> <!--BEGIN BACKGROUND--> <!-- Tu-22 Blinder Background --> <!--END BACKGROUND-->
Please note that your edits are only suggestions for changes and will
not
appear on the website unless approved by the webmaster!