Shvetsov ASh-73 Radial Aircraft Engine (1947–1957)
The
Shvetsov ASh-73 was an 18-cylinder, air-cooled, radial aircraft engine produced in the Soviet Union between 1947 and 1957. This engine served as the primary powerplant for the
Tupolev Tu-4, an unlicensed, reverse-engineered copy of the American
Boeing B-29 Superfortress.
Design and Development
The origins of the ASh-73 trace back to 1938, when a specification called for the development of an 18-cylinder, twin-row engine as an evolution of the Shvetsov M-25—a licensed Soviet production of the Wright R-1820-F3 Cyclone engine. The development progressed through several intermediate models, including the M-70, M-71, and M-72, all of which encountered significant engineering challenges before culminating in the successful ASh-73 design.
Contrary to some misconceptions, the ASh-73 was not a direct copy of the American Wright R-3350 Duplex-Cyclone, although both engines shared a common lineage through their Cyclone roots. Instead, the ASh-73 was an indigenous development designed to meet a similar specification. Some components of the ASh-73 were interchangeable with those of the R-3350, due to their shared ancestry and parallel design goals.
Initial development of the ASh-73 faced several hurdles, particularly with its progenitor, the M-70, which suffered from issues such as cracks in the master connecting rod, failures in the centrifugal supercharger's impeller, and burnt exhaust valves. The subsequent M-71, developed in 1939, overcame some of these issues but was delayed by World War II and never entered production due to limited manufacturing capacity. The M-72, an upgraded version of the M-71, was similarly sidelined as the ASh-73 became the focus of development.
Specifications and Features
First prototyped in 1945, the ASh-73 entered production in 1947. Early models lacked turbochargers, weighed approximately 1,330 kg (2,930 lb), and produced 2,400 horsepower (1,800 kW) during takeoff. The ASh-73TK variant introduced two TK-19 turbochargers and an intercooler—direct adaptations of American R-3350 components. Over its production run, the engine underwent multiple upgrades, including:
- Strengthening of the crankshaft, connecting rods, and pistons.
- Improvements to the accessory drive, reduction gearing, and exhaust valve seating.
- Lightening of pistons and enhancements to ignition systems.
The final production displacement of the ASh-73 was 58.122 liters (3,546.8 cubic inches), slightly larger than the R-3350’s 54.86 liters (3,347.9 cubic inches).
Advanced Variants
Several experimental versions of the ASh-73 were developed:
- The ASh-82TKF, a boosted model producing 2,720 hp (2,030 kW), which was bench-tested but not produced.
- The ASh-73TKFN, equipped with fuel injection and rated at 2,800 hp (2,100 kW), also remained a prototype.
- A turbo-compound version with a power-recovery turbine was conceived in 1949, but no further details are available.
Production and Legacy
The ASh-73 was produced primarily at
Factory No. 19, starting in 1947, with additional production at
Factory No. 36 in Rybinsk. Manufacturing continued until 1953 at Factory No. 19 and until 1957 at Factory No. 36, with a total of 14,310 engines built. Many of these engines were exported to the
People's Republic of China in the 1950s to support their fleet of Tu-4 bombers.
The Shvetsov ASh-73 remains a testament to the Soviet Union’s ability to adapt and advance aeronautical engineering, creating a powerplant that met the demands of post-war aviation.
Key Differences Between the ASh-73 and R-3350
- Development History:
- The R-3350 Duplex-Cyclone was an entirely American design by Wright Aeronautical, first developed in 1937. It was a cutting-edge engine with significant challenges early in its development, particularly with overheating and reliability. By the time of the B-29’s deployment, those issues had largely been resolved, and it became a highly successful engine.
- The ASh-73, on the other hand, was a Soviet design evolved from earlier Shvetsov engines such as the M-25 (a licensed Wright R-1820). While it was not a copy of the R-3350, it was developed to meet similar specifications and shared some features due to its Cyclone heritage.
- Design Characteristics:
- Both engines are 18-cylinder, twin-row, air-cooled radial engines.
- The R-3350 had a displacement of 54.86 liters (3,347.9 cubic inches), while the ASh-73 was slightly larger, with a displacement of 58.122 liters (3,546.8 cubic inches).
- The ASh-73 used components inspired by American designs but was independently developed to suit Soviet manufacturing techniques and requirements.
- Turbocharging:
- The R-3350 on the B-29 featured advanced turbosupercharging to maintain power at high altitudes, which was critical for strategic bombing missions.
- The ASh-73TK also included twin turbochargers and an intercooler, which were heavily inspired by the American R-3350 system. However, these components were direct adaptations rather than original designs.
- Applications:
- The R-3350 was primarily used in the B-29 and later aircraft like the Lockheed Constellation and Douglas DC-7.
- The ASh-73 was designed specifically for the Tupolev Tu-4, the Soviet reverse-engineered version of the B-29, but it also saw use in other Soviet designs.
- Production Methods:
- The ASh-73 reflects Soviet industrial priorities, favoring ruggedness and simplicity for mass production over cutting-edge performance. In contrast, the R-3350 represents the U.S. approach to maximizing performance through more advanced and intricate engineering.
Yes, the United States certainly has the ability to reverse-engineer the engines used in the Japanese A6M Zero series of aircraft, and here’s why:
Technical Capability
The A6M Zero’s engines, primarily the Nakajima Sakae series, were advanced for their time but are relatively simple by modern engineering standards. These engines were air-cooled, radial designs, featuring technologies that are well understood today. Modern manufacturing processes, such as precision CNC machining, advanced metallurgy, and 3D scanning, would make it feasible to recreate the components to exact specifications.
Furthermore, the United States has historically demonstrated the ability to reverse-engineer complex foreign technology, such as the Soviet MiG-25 "Foxbat" and even complete systems like the Soviet Buran space shuttle. Given these examples, reverse-engineering a WWII-era radial engine would not present a significant challenge to contemporary engineers.
Historical Precedent
During WWII, the U.S. examined and analyzed captured Japanese equipment extensively. The Zero itself was studied in detail after a mostly intact example crash-landed on Akutan Island in Alaska in 1942. Engineers used this captured plane to understand its strengths and weaknesses, which informed tactical and technical countermeasures. If reverse-engineering the Sakae engine had been deemed strategically important at the time, it could have been done.
Modern Challenges
While technically feasible, reverse-engineering a Zero engine today might face practical challenges:
- Lack of Original Blueprints: Without the original manufacturing data, recreating certain aspects of the engine (like exact tolerances or material compositions) would require extensive analysis of surviving engines.
- Material Obsolescence: Some of the materials used in the original engines may no longer be available or are no longer produced in the same way. Modern substitutes would likely be used, potentially altering performance slightly.
- Economic Feasibility: The effort to reverse-engineer and produce a small number of replica engines for historical aircraft would be extremely costly relative to the benefits, which is why many restored Zeros use substitute engines, like the Pratt & Whitney R-1830.
Conclusion
The United States has both the technical expertise and industrial capability to reverse-engineer the A6M Zero’s engines if desired. However, given the engine's relatively simple design by modern standards and the high cost of such an effort, the primary motivation for doing so would be for historical accuracy or specific restoration projects rather than for any practical application.