Mikulin AM-3

AM-3
Type	Turbojet
National origin	Soviet Union
Designer	Alexander Mikulin
Major applications	Tupolev Tu-16 Myasishchev M-4

The Mikulin AM-3 (also called RD-3M) was a turbojet engine developed in the Soviet Union by Alexander Mikulin.^[1]

Design and development

The development of the high-performance single-shaft engine began in 1948. The engine was used in different versions for the Tupolev Tu-16 and Tu-104, as well as the Myasishchev M-4. It had a single-stage low-pressure and an eight-stage high-pressure compressor, powered by a two-stage high-pressure turbine.

Variants

AM-3

first series version

AM-3A

AM-3D

Version for M-4 with 85.6 kN (19,200 lb_f) thrust

AM-3M-200

AM-3M-500, AM-3M-500A: developed further versions with 93.1 kN (20,900 lb_f)

WP-8

Chinese copy of the AM-3 with 93.1 kN (20,900 lb_f) thrust for the Xian H-6 (reproduction of the Tu-16)

Specifications

General characteristics

• Type: Turbojet engine
• Length: 5,380 mm (212 in)
• Diameter: 1,400 mm (55 in)
• Dry weight: 3,100 kg (6,800 lb)

Components

• Compressor: axial-flow, single stage LP, 8-stage HP
• Combustors: 14 x can combustion chambers
• Turbine: axial-flow, 2-stages

Performance

• Maximum thrust: 85.3 kN (19,200 lb_f)
• Overall pressure ratio: 6.4
• Turbine inlet temperature: 860°C
• Specific fuel consumption: 93.2 kg/(kN•h)
• Thrust-to-weight ratio: 2.81

See also

• Tumansky RD-9

Comparable engines

• Orenda Iroquois

Related lists

• List of aircraft engines

References

Wikimedia Commons has media related to Mikulin AM-3.

Notes

Bibliography

This page was last edited on 29 January 2024, at 15:29