Tu-214SUS (PU) Airborne communication center. First flight: 2010 © OAO Tupolev

Photo Tu-214SUS (PU) © OAO Tupolev


 Technical specifications      Photos      Video

 

 

This is a special missions plane equipped with advanced communication and navigational instruments in order to be able to communicate from any place it may be.

It was developed for use by the state head and other members of the government.

The Tu-214SUS (RA-64524) is the 11th aircraft of the Tu-204/214 family, which was admitted in the Russian presidential aircraft

 

Tu-214 SUS (PU) Airborne communication center. © Konstantinos Panitsidis

Tu-214 SUS (PU) Airborne communication center.

 


TECHNICAL SPECIFICATIONS

DESIGNER
OKB Tupolev
COUNTRY
Russia
TYPE
Airborne communication center
CREW
-
POWER-PLANT
Two engine bypass engine PS-90A
Thrust, kgf
2 x 16.000
DIMENSIONS
 
Length, m
46,20
Height, m
13,90
Wing span, m
42,00
Wing area, m2
182,40
WEIGHT
 
Empty aircraft, kg
59.000
Normal take-off, kg
-
Maximum take-off, kg
110.750
Internal fuel, kg
-
PERFORMANCE
 
Maximum speed, km/h
-
Cruising speed, km/h
850
Range, km
6.500
Service ceiling, m
12.000