Antonov An-72 Article Index for
Antonov
 

Information About

Antonov An-72






Designed as a STOL transport, the Antonov An-72 ( NATO Reporting Name '''''Coaler''''') was intended as a replacement for the An-26 , but variants have found success as commercial freighters. Produced in tandem with the An-72, the '''Antonov An-74''' variant adds the ability to operate in harsh weather conditions in polar regions. Other An-72 versions include the '''An-72S''' VIP transport and '''An-72P''' maritime Patrol Aircraft . Also been used in the Sahara desert to land on temporary landing
fields during the Paris-Dakar rally.

An interesting design feature of the An-72 and An-74 is the use of the Coandă Effect to improve STOL performance, utilizing engine exhaust gases blown over the wing's upper surface to boost lift. The first flight was made in August 31, 1977 , but went into the 80s until production started. The power plant used is ZMKB Progress D36. The freighter can travel at a speed of 330 kt (611 km/h, 0.50 mach).

The An-72 bears similar resemblance to an earlier aircraft, the experimental Boeing YC-14 . Boeing may introduce the An-72 as a new option for the United States Army 's pending Future Cargo Aircraft (FCA) competition. Were Boeing to offer it, the An-72 would be the only jet-powered aircraft in the competition.

As an interesting sidenote, the An-72 is often called ''cheburashka'' by Russians beause with its large intake ducts located close to the fuselage, it resembles Cheburashka , a very popular animated creature in Russian cartoons.


IMAGES



SPECIFICATIONS (AN-72)


  plane Or Copter plane
  jet Or Prop jet
  crew 3
  capacity 32-68 passengers
  length Main 2658 m
  length Alt 87 ft 2 in
  span Main 2583 m
  span Alt 84 ft 9 in
  height Main 824 m
  height Alt 27 ft 0 in
  area Main m&2
  area Alt ft&2
  empty Weight Main 7,500 kg
  empty Weight Alt 16,500 lb
  loaded Weight Main 19,050 kg 10,000 kg with 30 min reserve of fuel
  loaded Weight Alt 42,000 lb / 22,000 lb
  max Takeoff Weight Main 33,000 kg
  max Takeoff Weight Alt 72,750 lb
  engine (jet) Lotarev D-36
  type Of Jet Turbofan s
  number Of Jets 2
  thrust Main 637 KN
  thrust Alt 14,300 Lbf
  max Speed Main 705 km/h
  max Speed Alt 438 mph
  cruise Speed Main 550-600 km/h at 10,000 m
  cruise Speed Alt 342-373 mph at 32,800 ft
  range Main 4,800 km
  range Alt 2,980 mi
  ceiling Main 11,800 m
  ceiling Alt 38,715 ft
  climb Rate Main m/s
  climb Rate Alt ft/min
  loading Main kg/m&2
  loading Alt lb/ft&2



RELATED CONTENT