Tsumansuki R-29

R-29-300

Tsumansuki R-29 Was developed by the early 1970's for aviation. It is described as a "third generation" Soviet overall with adopted air-cooled turbine blade with high thrust weight ratio.

table of contents

Derived type

R-29-300

The prototype was used for MiG - 23 MF and its derivative models.

R-29B-200

Simplified engine for MiG - 27.

R-29 PN

It was advanced advanced derived type and was replaced by non export type -300.

R-29 BS-300

Modified gearbox. It was used for export type Su - 17 (Su - 22).

R-29T-300

An engine mounted instead of the prototype T6 - 8D. It was not adopted because the flight characteristics were bad.

WP-15

Type in China. In August 1978 China received a fighter plane in return for selling at a friendly price (then only 1 million). In parallel with the analysis of the aircraft on March 10, 1979, we instructed the 601 laboratory to study whether the R - 29 engine that the aircraft was carrying was domestically produced by the method and can be loaded. As a result of the examination, it was estimated that the performance of the aircraft () to be installed is more reliable than the one that was difficult to develop, and in terms of practical application, it was officially selected as the engine of J-13 in May 1980 It was done. However, reliability problems could not be solved, and in March 1981 the development with the aircraft was discontinued.

Mounting machine

• () (Developed for this aircraft)
• • • () *

Specification data

General characteristics

format:* *Total length:4,991 mm (196.5 in) Diameter:*968 mm (38.1 in) *Dry Weight:1,760 kg (3,900 lb)

Component

Compressor:*Low pressure 5 stages, high pressure 6 stages (axial flow type) :annular type :**High pressure 2 steps, low pressure 1 step

Performance

:*When using afterburner 12,480 kg (27,500 lb) (9, 900 kg (22,000 lb) when afterburner is not used) *():12.9: 1 Air flow rate:*105 kg / s *:

_ Source: _ Gunston

Related item

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Similar engine

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Source

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Footnote

1. *Gunston 1989, p. 168. 2. Sosounov, VA (1990). The Development of Aircraft Power Plant Construction in the USSR and the 60 th Anniversary of CIAM. AlAA / ASME / SAE / ASEE 26th Joint Propulsion Conference, July 16-18, 1990. Orlando , Florida. AIAA-90-2761. 3. ^. Janes Aero Engines. Edited: 1 April 2010. Retrieved: 8 September 2010. Four. * Five.

Document

• Gunston, Bill. World Encyclopaedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.

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Post Date : 2018-01-30 08:00

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