The S-80PT, a patrol-transport version
of the S-80 aircraft, the Emergency Situation Ministry
and Boarder Guard Service of Russian
Federation showed their interested in, is capable
of all-weather round-the-clock missions
patrolling sea and ground borderlines for 6-9
hours. In addition, this version is capable of giving a lift to troops and materiel, airdrop of troops
and cargo, pipeline inspection, ice drift control,
search and rescue missions.
The patrol/transport version of the S-80
aircraft is equipped with a Strizh on-board complex
(developed by the Leninets holding company)
which includes multifunctional all-round looking
radar installed in the forebody and infrared
imaging equipment. The Strizh complex allows
acquisition of ship-type targets at ranges up
to 220 km and location of a man aboard inflatable life raft at distances up to 1.5-2 km. Via
special-purpose radio channel interception
groups, combat units or rescue teams can be
guided to the located air, sea or ground targets.
On-board arrangement of Strizh complex
components provides for a usage of inner space
for solution of respective tasks (particularly,
housing 20 parachutists or paratroopers).
The S-80PT is fitted with a container-
installed gun located under the fuselage. Four
undenting suspension units can accommodate
guided 'air-to-surface', 'air-to-air' missiles and
unguided missile modules.
Description | |
---|---|
Design | AOOT "OKB Sukhoi" |
Type | S-80PT |
Year | 2000 |
Function | patrol-transport aircraft |
Crew | 2 |
Paratroopers | 20 |
Dimensions & Weight | |
Wingspan, m | 23,16 |
Length, m | 17,85 |
Overall height, m | 5,58 |
Wing area, sq.m. | 44 |
Maximal takeoff weight, kg | 12500 |
Maximal payload, kg | 3000 |
Fuel weight, kg ( litr ) | 2350 (2500) |
Power-plant | |
Engines | turboprpp GE CT-9B |
Power, h.p. (kWt) | 2х 1870 |
Performance (project) | |
Cruising speed, km/h | 510 |
Operating range with 1560 kg load, km | 2475 |
Ferry range, км | 2890 |
Time of a loitering of an airplane, hours | 10-12 |
Practical seiling, m | 8000 |
Cruising altitude, m | 6000 |
Takeoff run (Gmax, MCA, H=0m), m | 555 |
Landing roll (with braking and reverse of propeller), m | 280 |
References and Credits: