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Shvetsov ASh-62

radial piston aircraft engine

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Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionApr 14, 2026
Entity authorityQ669734 ↗
Source-derived summary

The Shvetsov ASh-62 (Russian: Швецов АШ-62, designated M-62 before 1941) is a nine-cylinder, air-cooled, radial aircraft engine produced in the Soviet Union. A version of this engine is produced in Poland as the ASz-62 and the People's Republic of China as the HS-5.

Design and development

The ASh-62 was a development of the Wright R-1820 Cyclone that had been built in Russia under licence as the Shvetsov M-25, the main improvements including a two-speed supercharger and a more efficient induction system. Power was increased from the Cyclone's 775 hp to 1,000 hp. First run in 1937, licensed versions are still in production by WSK "PZL-Kalisz" in Poland (as of 2017). The Ash-62 was also produced in China. It is estimated that 40,361 were produced in the USSR.

Polish-built ASz-62IR engines (Polish transcription of Russian name), by WSK "PZL-Kalisz" in Kalisz, are compatible with FAR-33 requirements. Further developments in Poland are the K9-AA, K9-BA and K9-BB engines, with take-off power of 1178 hp (860 kW), indicated power 698 kW. From 2015 the ASz-62IR-16E was produced with electronic fuel injection, offering greater power and the possibility of running on commercial automotive fuel.

The M-63 was an improved version of the M-62 with the power output increased to 821 kW (1,100 hp) at 2,300 rpm for takeoff and 671 kW (900 hp) at 2,200 rpm at 4,500 m (14,800 ft) due to a higher compression ratio of 7.2:1 and a higher redline.

Applications

Antonov An-2

Antonov An-6

Beriev Be-4

Lisunov Li-2

Kharkiv KhAI-5

Polikarpov I-153

Polikarpov I-16

PZL-106 Kruk (some variants)

PZL-Mielec M-18 Dromader

PZL M-24 Dromader Super (K-9AA)

Sukhoi Su-2 (prototype)

Sukhoi Su-12

VL Myrsky (one prototype)

Specifications (M-62)

Data from Liss.

Editorial summary

This brief starts where responsible research should: with the source description of “Shvetsov ASh-62” as radial piston aircraft engine. Everything that follows is an evidence route, not borrowed authority.

Editorial reviewA concise reference frame for defining the subject, testing terminology and identifying the institution closest to the evidence. The current lead gives the account dated anchors—1941, 1820, 1937, 2017—that can be checked directly. The selected authority fields contribute no independent date. The account is most persuasive where Shvetsov, ASh-62 and radial can be independently traced.
Editorial analysis

Why this record matters

The subject matters to the general reference register because the source frames it as radial piston aircraft engine. Its deeper value depends on whether names, dates, institutions and citations support that framing.

Evidence profile

The citation trail is more important than the brevity of the summary: it shows where individual claims can be examined in context. The source revision retrieved here is dated Apr 14, 2026. The linked authority identifier is Q669734. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1941, 1820, 1937 and 2017.

Critical limits

The absence of detail may reflect summary conventions rather than a lack of surviving documentation. The source lead contains qualifying language; that uncertainty should survive quotation, summary and reuse. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

How to read it

Use the entry as an orientation point, then follow its citations and revision history. Names, dates and institutional relationships should be checked against the original record.

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Source & attribution

This entry incorporates text from “Shvetsov ASh-62” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.