Myasishchev Design Bureau M-17 Stratosfera

Fixed Wing Single Engine

Picture of Myasishchev Design Bureau M-17 Stratosfera

Aircraft Information

ICAO Code
M17
Manufacturer
Myasishchev Design Bureau
Model
M-17 Stratosfera
Aircraft Type
Fixed Wing Single Engine
Primary Role
Interceptor

Technical Data

Engine Type
Turbojet
Engine Model
Kolesov RD-36-51V
Production Years
1978-1987
Units Produced
2 prototypes
First Flight
1982-05-26
Notable Operators
Soviet Air Force, Research institutions

The Myasishchev M-17 Stratosfera was a specialized high-altitude interceptor designed to counter American reconnaissance balloons during the Cold War. First flown in 1982, it was a twin-boom aircraft powered by a single Kolesov RD-36-51V turbojet engine capable of reaching altitudes exceeding 71,000 feet. With its distinctive anhedral wings and 18,400-kilogram maximum takeoff weight, only two prototypes were built by Vladimir Myasishchev's design bureau before the program evolved into the more successful M-55 Geophysica.

Origins and Design Challenge

The M-17's development traced back to the 1950s when Soviet air defenses struggled against American high-altitude reconnaissance platforms. Vladimir Myasishchev's design bureau faced an unprecedented engineering challenge: creating an aircraft capable of intercepting reconnaissance balloons and the Lockheed U-2 at stratospheric altitudes where conventional fighters could not operate effectively.

The original concept, designated Subject 34 and nicknamed "Chaika" (Seagull), featured a twin-boom configuration with anhedral wings. This unusual design emerged from necessity rather than aesthetics. The Central Aerohydrodynamic Institute (TsAGI) discovered that none of their extensive wing profile library could provide adequate lift coefficients in the thin stratospheric atmosphere, forcing engineers to develop entirely new aerodynamic solutions.

Troubled Development and Production

Production began at the Kumertau plant in 1978, where the facility normally manufactured Ka-26 agricultural helicopters. The first M-17 prototype met a tragic end during December 1978 when test pilot attempted to avoid a collision with snow during near-zero visibility conditions, ultimately striking an almost-invisible hill and killing the pilot.

Following this disaster, production transferred to the Smolensk facility. The second aircraft, bearing civil registration CCCP-17103 and Aeroflot markings, completed its first flight on May 26, 1982, with Eduard Cheltsov at the controls. A third aircraft, CCCP-17401, was subsequently completed, though the entire balloon-interceptor program faced termination by 1987.

Revolutionary Powerplant

The M-17's heart was the Kolesov RD-36-51V turbojet, a non-afterburning engine derived from the Tu-144 supersonic transport's powerplant. Producing 68.6 kilonewtons of thrust, this Rybinsk-manufactured engine represented the most powerful Soviet turbojet available for the application. However, the aircraft's operational limitations became apparent during testing: while capable of rapid climbs to extreme altitudes, the M-17's endurance was restricted to merely two hours, contrasting sharply with the U-2's ability to conduct extended reconnaissance missions.

Technical Challenges and NATO Recognition

Flight testing revealed significant aerodynamic problems that plagued the M-17 throughout its development. Engineers struggled with tail vibrations during high-speed flight at altitude, unacceptably high control surface loads, and ineffective airbrakes. By the time these issues were resolved, military priorities had shifted toward different anti-balloon weapons systems.

Despite these challenges, NATO assigned the reporting name "Mystic-A" to the M-17, acknowledging its potential threat to Western reconnaissance operations.

Record-Breaking Performance

The M-17's high-altitude capabilities were definitively demonstrated on March 28, 1990, when Vladimir V. Arkhipenko piloted CCCP-17401 to an altitude record of 21,830 meters (71,620 feet) in the C-1i weight class for landplanes between 16,000 and 20,000 kilograms takeoff weight. The aircraft ultimately established twelve Fédération Aéronautique Internationale World Records, with five still standing today.

Scientific Mission and Antarctic Research

Rather than serving as an interceptor, the M-17 found new purpose in scientific research. In 1992, the aircraft conducted ozone layer investigations over Antarctica, demonstrating its value for high-altitude atmospheric research rather than military operations.

Evolution to the M-55 Geophysica

The M-17's legacy lived on through its successor, the M-55 Geophysica (NATO designation "Mystic-B"), which first flew on August 16, 1988, again with Eduard Cheltsov as pilot. The M-55 featured twin Soloviev D-30-10V turbofan engines producing 49 kilonewtons each, a longer fuselage, shorter wings, and dramatically improved endurance of 6.5 hours compared to the M-17's two-hour limitation.

Measuring 23 meters in length with a wingspan exceeding 37 meters, the M-55 achieved a cruise speed of 750 kilometers per hour while maintaining the extreme altitude capabilities of its predecessor. Victor Vasenkov demonstrated these capabilities on September 21, 1993, reaching 21,360 meters in the C-1j class, establishing another record that remains unbroken.

Current Status and Museum Display

The M-17 program represented both the ambition and limitations of Soviet high-altitude aircraft development. While only two prototypes were completed before program termination, the design's influence continued through the M-55 Geophysica, which remains active in atmospheric research roles. One M-55 prototype bearing Aeroflot markings is preserved at the Air Force Museum at Monino, serving as a testament to Myasishchev's innovative approach to stratospheric flight challenges.