SU-24
The Sukhoi Su-24 is a supersonic, all-weather attack aircraft developed in the Soviet Union. The aircraft has a variable-sweep wing, twin-engines and a side-by-side seating arrangement for its crew of two. It was the first of the USSR's aircraft to carry an integrated digital navigation/attack system.
Type
Role
Country of Origin
Introduction
Note
The Su-24 has two Saturn/Lyulka AL-21F-3A after-burning turbojet engines with 109.8 kN (24,700 lbs) thrust each, fed with air from two rectangular side-mounted intakes with splitter plates/boundary-layer diverters.
In early Su-24 ("Fencer A" according to NATO) aircraft these intakes had variable ramps, allowing a maximum speed of 2,320 kilometers per hour (1,440 mph), Mach 2.18, at altitude and a ceiling of 17,500 meters (57,400 ft). Because the Su-24 is used almost exclusively for low-level missions, the actuators for the variable intakes were deleted to reduce weight and maintenance. The earliest Su-24 had a box-like rear fuselage, which was soon changed in production to a rear exhaust shroud more closely shaped around the engines in order to reduce drag.
Crew: 2 (pilot and navigator)
Length: 22.67m
Height: 5.92m
Swept Wingspan: 10.36m
Extended Wingspan: 17.63m
Normal Take-Off Weight: 35,910kg
Maximum Take-Off Weight: 39,700kg
Normal Combat Load: 3,000kg
Landing Roll: 800m to 850m
Maximum Combat Load: 8,000kg
Fuel Capacity, Internal Fuel Tanks: 9,850kg
Fuel Capacity With 3 External Fuel Tanks: 16,460kg
Ferry Range With External Fuel Tanks: 3,055km
Maximum Speed Near Ground: 1,340km/hr
Maximum Speed at an Altitude of 11km: 1,550km/h
Service Ceiling: 11,000m
Take-Off Run: 850m to 900m
Landing Roll: 800m to 850m
Type of packaging
Quantity per pack
Number in a wooden case
Dimensions of a wooden case
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Weight of wooden case
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UN Number
Hazard Class
SU-24
Description
Type
Role
Country of Origin
Introduction
Note
The Sukhoi Su-24 is a supersonic, all-weather attack aircraft developed in the Soviet Union. The aircraft has a variable-sweep wing, twin-engines and a side-by-side seating arrangement for its crew of two. It was the first of the USSR's aircraft to carry an integrated digital navigation/attack system.
The Su-24 has two Saturn/Lyulka AL-21F-3A after-burning turbojet engines with 109.8 kN (24,700 lbs) thrust each, fed with air from two rectangular side-mounted intakes with splitter plates/boundary-layer diverters.
In early Su-24 ("Fencer A" according to NATO) aircraft these intakes had variable ramps, allowing a maximum speed of 2,320 kilometers per hour (1,440 mph), Mach 2.18, at altitude and a ceiling of 17,500 meters (57,400 ft). Because the Su-24 is used almost exclusively for low-level missions, the actuators for the variable intakes were deleted to reduce weight and maintenance. The earliest Su-24 had a box-like rear fuselage, which was soon changed in production to a rear exhaust shroud more closely shaped around the engines in order to reduce drag.
Technical data and Packaging
Crew: 2 (pilot and navigator)
Length: 22.67m
Height: 5.92m
Swept Wingspan: 10.36m
Extended Wingspan: 17.63m
Normal Take-Off Weight: 35,910kg
Maximum Take-Off Weight: 39,700kg
Normal Combat Load: 3,000kg
Landing Roll: 800m to 850m
Maximum Combat Load: 8,000kg
Fuel Capacity, Internal Fuel Tanks: 9,850kg
Fuel Capacity With 3 External Fuel Tanks: 16,460kg
Ferry Range With External Fuel Tanks: 3,055km
Maximum Speed Near Ground: 1,340km/hr
Maximum Speed at an Altitude of 11km: 1,550km/h
Service Ceiling: 11,000m
Take-Off Run: 850m to 900m
Landing Roll: 800m to 850m
Type of packaging
Quantity per pack
Number in a wooden case
Dimensions of a wooden case
Weight of the package
Weight of wooden case
Weight
Volume m3
UN Number
Hazard Class
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