Tag Archives: Mikoyan-Gurevich MiG 17

22 November 1955

Tupolev Tu-16 (NATO codename "Badger")
Tupolev Tu-16 (NATO codename “Badger”). (Federation of American Scientists)
Major Fedor Pavlovich Golovashko, Hero of the Soviet Union.
Major Fedor Pavlovich Golovashko, Hero of the Soviet Union (1923–1981)

22 November 1955:  The Soviet Union’s first thermonuclear weapon, RDS-37, was air-dropped at the Semipalatinsk Test Site, approximately 150 kilometers west of the city of Semipalatinsk, Kazakh S.S.R. (now, Kazakhstan). The bomber, a Tupolev Tu-16A, and its crew were under the command of Senior Test Pilot Major Fedor Pavlovich Golovashko.

The RDS-37 was a two-stage radiation-implosion thermonuclear bomb, what was called at the time a “hydrogen bomb.” (RDS stands for Rossiya delaet sama—meaning, in effect, that “Russia does it itself.” This three-letter prefix was applied to atomic tests since the first, RDS-1, 29 August 1949.)

This was the Soviet Union’s twenty-fourth nuclear weapons test, but its first true thermonuclear bomb, and it was the world’s first air-dropped “H bomb.” (The United States’ first air-drop of a thermonuclear weapon, Redwing Cherokee, took place six months later, 20 May 1956. Great Britain’s Grapple I/Short Granite test occurred 15 May 1957.)

Major Golovashko and his crew had made a previous attempt with the RDS-37. Two days earlier, 19 November, the loading of the bomb began at 6:45 a.m. Four hoists were used to lift it into the bomber’s weapons bay. The process took about two hours.

In this still frame from a cine film recording, the RDS-37 bomb is shown being positioned under the Tupolev Tu-16A bomber for loading into the bomb bay. (Pravda.net)

At 9:30 a.m., the Tu-16 took off from Zhana Semey Airport (PLX), about 8 kilometers (5 miles) south of the city of Semipaltinsk. It began climbing to an altitude of 12,000 meters (39,370 feet) as it flew toward the test site. Golovashko’s bomber was escorted by pairs of Mikoyan-Gurevich MiG-17 fighters to prevent the theft of the test weapon.

Although the weather had been forecast to be good, it unexpectedly began to deteriorate. The Tu-16 was above a cloud layer with the test area obscured. As the crew prepared to bomb by radar, the radar equipment failed and all attempts to repair it were unsuccessful.

Test conductors were very concerned about landing the Tupolev back at Semipalatinsk with a fully-armed nuclear bomb still on board. There was consideration of dropping the RDS-37 over remote mountains, but there was no certainty of being able to avoid villages or towns, and if the bomb were to only partially detonate there could be widespread contamination by its radioactive fuel.

There was a delay in making a decision and the Tupolev’s fuel was getting low. Finally it was decided to have the bomber return to Semipalatinsk with the bomb. The landing was uneventful and the technicians removed the RDS-37 for servicing before the next test attempt.

Андре́й Дми́триевич Са́харов

It was normal procedure for bomber crews to rotate, but the decision was made to have Major Golovashko’s crew make the second test flight. On 22 November the weapon loading began at 4:50 a.m., with takeoff at 8:34 a.m. Again the Tupolev Tu-16A was escorted by pairs of MiG-17s. Once again, the bomber arrived over the test site at 12,000 meters, flying at 870 kilometers per hour (541 miles per hour).

Soviet nuclear weapons designer Andrei Dmitrievich Sakaharov, whose “other idea”—radiation-implosion—was used in the design of the RDS-37, was at an observation site about 70 kilometers from the test target. He watched the Tu-16 as it flew overhead and described it as, “dazzling white with its sweptback wings and slender fuselage extending far forward, it looked like a sinister predator poised to strike.” He also noted that the color white is “often associated with death.”

Sakharov's "white bomber."
Sakharov’s “sinister predator.”

After being released from Major Golovashko’s Tupolev, the RDS-37 was retarded by parachute to allow time for the bomber to get away. It detonated at 1,550 meters (5,085 feet) above the ground. The flight crew described seeing a blue-white flash that lasted 10 to 12 seconds. The shock wave of the detonation, spreading at the speed of sound, hit the bomber 3 minutes, 44 seconds after the drop. The Tu-16 experienced accelerations of 2.5Gs, and was lifted to higher altitude. It was not damaged.

5–7 minutes following the detonation the distinctive mushroom cloud had reached to a height of 13–14 kilometers (8–8.7 miles) and its diameter was 25–30 kilometers (15.5–18.6 miles).

The RDS-37 detonated with a reported yield varying between 1.6 and 1.9 megatons (depending on source). The bomb had a designed yield of 3 megatons but this had been intentionally reduced for this test.

The bomb detonated under a temperature inversion layer which reflected a large proportion of the explosive force back to the ground. A small town about 75 kilometers (47 miles) away suffered significant destruction. A small child was killed when a building collapsed. At another location, a soldier in an observation was killed when the trench caved in from the shock. Nearly 50 others were injured. Windows were broken as far as 200 kilometers (124 miles) away.

Several videos of this test are available on YouTube.

The Tu-16 has a normal bomb load of 3,000 kilograms (6,614 pounds), but can carry up to 9,000 kilograms (19,842 pounds). It has seven Afanasev Makarov AM-23 23mm autocannons for defense, mounted in three pairs which are remotely operated by the gunners, and a single gun in the nose. These guns fire at a rate of 900 rounds per minute.

The Tupolev Tu-16 was built in bomber, cruise missile carrier, electronic counter measures, aerial tanker, and electronic and photographic reconnaissance versions, at three factories in the Soviet Union: Kazan Plant N22, Kuibyshev N18 and Voronezh N64. 1,507 Tu-16s were built before production ended in 1961. 453 of these were the Tu-16A nuclear weapons version. Another 120 were built under license in China by Harbin Aircraft. These are designated H-6.

Фёдор Павлович Головашко

Fedor Pavlovich Golovashko was born at Byokovo, Novosibirsk, 22 June 1923. He was educated through the 9th grade before being drafted into the Soviet Army in 1941. He was trained as a pilot at the Novosibirsk Military Aviation School, graduating in 1943.

He was assigned to a Long Range Aviation regiment (Dalnyaya Aviatsiya) under the command of Alexander Ignatyevich Molodchy, twice a Hero of the Soviet Union.

Golovashko’s final missions of the Great Patriotic War (World War II) were flown against Berlin.

Fedor Golovashko remained in the Air Force following the war and soon was in command of a squadron. He became a test pilot in 1954 and was assigned to the Semipalatinsk Test Site.

Senior Test Pilot Major Fedor Pavlovich Gorovashko was named a Hero of the Soviet Union, 11 September 1956. He reached the rank of Colonel before retiring from the Air Force in 1961. He had been awarded the Order of Lenin, Order of the Red Banner (two awards), Order of the Patriotic War 1st Degree, and the Order of the Red Star (two awards).

After retiring, Colonel Golovashko lived in Odessa. He died there, 19 April 1981.

Major Golovashko’s bomber was a Tupolev Tu-16A (NATO codename “Badger-A”). This was a two-engine turbojet-powered long-range medium bomber. It was normally operated by a flight crew of seven.

OKB Tupolev test pilot Nikolai Stepanovich Rybko, Hero of the Soviet Union (1911–1977)

Developed from the Tupolev Design Bureau Project 88, the prototype Tu-16 made it’s first flight at Zhukovsky Airfield (Ramenskoye Airport), southeast of Moscow, on 27 April 1952. The test pilot was Nikolai Stepanovich Rybko. This was the Soviet Union’s first swept-wing bomber. It was designated Tu-16 and entered production in 1954.

The Tu-16A was designed specifically to carry nuclear weapons and had a strengthened fuselage and heated bomb bay. The Tupolev Tu-16 is 34.8 meters (114.2 feet) long with a wingspan of 33 meters (108.3 feet) and overall height of 10.36 meters (34 feet). The wings are mounted at mid-fuselage and have a compound sweep. The inner portion has a leading edge sweep of 40.5°, and the outer wing is swept to 35°. t has an empty weight of 37,200 kilograms (82,012 pounds) and maximum takeoff weight of 79,000 kilograms (174,165 pounds).

Power is supplied by two large turbojet engines mounted in the wings at the fuselage, similar to the de Havilland Comet, though they are angled slightly outward to direct the exhaust away from the airplane’s skin panels. The Tu-16A variant is equipped with two Mikulin RD-3M-200 turbojets which produce 21,835 pounds of thrust, each.

The Tu-16A has a maximum speed of 992 kilometers per hour (610 miles per hour) and a service ceiling of 12,800 meters (41,995 feet). Its maximum range is 6,400 kilometers (3,977 miles).

Screen Shot 2015-11-21 at 16.05.37 © 2017, Bryan R. Swopes

2 September 1958, 1313–1314 UTC

Gun Camera image from Senior Lieutenant Kucheryaev’s MiG 17. (PVO Strany)

During the Cold War, the United States routinely flew reconnaissance missions around and over Soviet Bloc territory, including over the Soviet Union itself. There have been unconfirmed reports that as many as 40 U.S. aircraft were shot down, and more than 200 airmen killed. Several hundred more may have been captured and held as prisoners.

2 September 1958: A U.S. Air Force Lockheed C-130A-II Dreamboat, 56-0528 (MSN 182-3136) of the 7406th Support Squadron, based at Rhein-Main Air Base, near Frankfurt am Main, Germany, was on a clandestine reconnaissance mission near the Union of Soviet Socialist Republics (USSR) border with Armenia (a Soviet Block nation). The C-130 had departed from the U.S. air base at Incirlik, Turkey. In addition to the 6-man flight crew, the aircraft carried 11 radio operators and technicians from the 6911th Radio Group, Mobile.

Two 11th Air Army Mikoyan-Gurevich MiG 17s (NATO code name: “Fresco”), part of the Tbilisi Air Defense District, were dispatched from Leninakan (now known as Gyumri) to intercept and destroy the C-130. The radar interecept was controlled from Leninakan by Captain Romanyuta.

When the two fighters, piloted by Senior Lieutenant Kucheryaev (201) and Senior Lieutenant Ivanov (218), were delayed for 7 minutes by a dust storm, two more MiG 17s, piloted by Senior Lieutenant Lopatokov (582) and Lieutenat Gavrilov (583), were launched from Yerevan, the capital city of Armenia. (U.S.  radar tracking reports indicate that 201 and 218 were airborne at 1152Z.) The weather was reported as good, with 2/10ths to 3/10ths (scattered) cloud cover.

The fighters closed on the C-130 and reported that it was flying at an altitude of 9,000–10,000 meters (29,528–32,808 feet). At 1213Z the fighters reported the C-130 at 10,000 meters (32,808 feet). Lieutenants Lopatokov and Gavrilov each made firing passes, with Gavrilov reporting that he fired three bursts. Next, Lieutenants Kucheryaev and Ivanov attacked. Lieutenant Kucheryaev reported that the C-130 started burning after his third burst. Lopatokov and Gavrilov attacked again.

Gun camera image of the shootdown of U.S. Air Force Lockheed C-130A-II, 56 0528, 2 September 1958. (ПВО страны [protivovozdushnaya oborona strany, or PVO Strany])
The C-130 caught fire and its tail was observed to fall of. None of the fighter pilots observed any parachutes from the transport. 56-0528 crashed near N. 40°23′, E. 43° 55′. All 17 crewmen aboard were killed.

All four MiG 17s returned to the fighter base at Leninakan.

Reported location of C-130 shoot down. (Google Maps)

The Soviet radio communications during the intercept were heard by U.S. communications intelligence personnel.

News reports of the interecept appeared in Советская Авиа (Sovetskaya Aviatsiya) 19–29 September 1958.

(Arlington National Cemetery)

The remains of six of the air crew were returned to the United States.

“A replica of 56-0528, a C-130A-II “Sun Valley” reconnaissance aircraft shot down over Armenia on 2 September 1958, on display at the National Cryptologic Museum, Fort Meade, Maryland (real identity – C-130A-45-LM, c/n 3160, s/n 57-0453).”

56-0528 was a Lockheed C-130A-8-LM Hercules which had been converted to a C-130A-II Dreamboat electronic surveillance configuration by the Texas Engineering & Manufacturing Company (TEMCO) under Project SUN VALLEY. It was flown by two pilots with a navigator and radar navigator, a flight engineer and scanner. There were ten radio operators and a radio repair technician.

The cargo compartment had been converted to three radio compartments. The two forward compartments each had voice intercept positions for four operators, while the third had only two. A galley and radio repair station were at the rear. There was an airline-style toilet. The aft cargo doors were permanently closed and sealed. Radio antennas were installed in fiberglass pods resembling fuel tanks, mounted between the inboard and outboard engines. In the aircraft’s nose was the AN/APN-59 navigation, search, and weather radar. The aircraft was equipped with four alternators to supply electrical power for the equipment.

The Lockheed C-130A Hercules is a four-engine high-wing transport. It was normally operated by a crew of four. The C-130A was 97.8 feet (29.81 meters) long with a wingspan of 132.6 feet (40.42 meters), and height of 38.1 feet (11.61 meters). The total wing area was 1,745.5 square feet (162.16 square meters). The transport’s empty weight was 59,164 pounds (26,836 kilograms) and takeoff weight, 122,245 pounds (55,449 kilograms).

The C 130 has a rear loading ramp for vehicles, and there is a large cargo door on the left side of the fuselage, forward of the wing, The transport’s cargo compartment volume is 3,708 cubic feet (105.0 cubic meters). It could carry 35,000 pounds (15,876 kilograms) of cargo.

The C-130A was equipped with four Allison T56-A-1A turboshaft engines, driving three-bladed propellers. The engines produced 3,094 shaft horsepower at 13,820 r.p.m. (continuous), and 3,460 horsepower, Military Power (30-minute limit) or Takeoff ( 5-minute limit).

The C-130A had a cruise speed of 286 knots (329 miles per hour/530 kilometers per hour) and maximum speed of 326 knots (375 miles per hour/604 kilometers per hour) at 24,200 feet (7,376 meters). Its range with a 35,000 pound (15,876 kilograms) payload was 1,835 nautical miles (2,112 statute miles/3,398 kilometers). The initial rate of climb at Sea Level was 4,320 feet per minute (21.95 meters per second). The combat ceiling was 38,700 feet (11,796 meters).

In addition to its basic role as a transport, the C-130 has also been used as an aerial tanker, a command-and-control aircraft, weather reconnaissance, search and rescue, and tactical gunship. It has even been used as a bomber, carrying huge “Daisy Cutters” to clear large areas of jungle for use as helicopter landing zones, or, more recently, the Massive Ordnance Air Blast “mother of all bombs.” The aircraft has been so versatile that it has served in every type of mission. Over 40 variants have been built by Lockheed, including civilian transports. It is in service worldwide.

The prototype YC-130 first flew 23 August 1954. The first production C-130A made ts first flight 7 April 1955. The latest version is the Lockheed C-130J Hercules. After 69 years, the C-130 is still in production, longer than any other aircraft type.

Mikoyan-Gurevich MiG-17. (Mikoyan-Gurevich Design Bureau)

The Mikoyan-Gurevich MiG 17 is an improved version of the MiG-15 fighter. It is a single-place, single-engine, swept-wing, high-subsonic interceptor.

The MiG 17’s wing is thinner, stiffer, and more highly swept than the wing of the MiG 15. There are three stall fences on the upper surface of each wing. The wings are mounted at mid-fuselage with -3° anhedral. The leading edges of the inboard sections ares swept aft to 45° while the outboard sections are swept 42°.

Mikoyan-Gurevich MiG-17. (Mikoyan-Gurevich Design Bureau)

The MiG 17 is 11.364 meters (37 feet, 3.4 inches) long, with a wingspan of 9.600 meters (31 feet, 5.95 inches), and height of 3.800 meters (12 feet, 5.6 inches). It has an empty weight o f3,939 kilograms (8,684 pounds). The normal takeoff weight is 5,340 kilograms (11,773 pounds), and the maximum takeoff weight (MTOW) is 6,069 kilograms (13,380 pounds).

Mikoyan-Gurevich MiG-17 three-view illustration with dimensions.

The MiG 17 is powered by a Klimov VK-1F centrifugal-flow turbojet. The basic VK-1 was developed from the Rolls-Royce Nene. The British engines were reverse-engineered by Vladimir Yakovlevich Klimov and manufactured at Factory No. 45 in Moscow as the Klimov VK-1. The VK-1 had a single-stage centrifugal-flow compressor, 9 combustion chambers and a single-stage axial-flow turbine. It produced a maximum 26.48 kilonewtons of thrust (5,952 pounds of thrust). The VK-1 was 2.600 meters (8 feet, 6.4 inches) long, 1.300 meters (4 feet, 3.2 inches) in diameter, and weighed 872 kilograms (1,922 pounds).

Mikoyan-Gurevich MiG-17. (Mikoyan-Gurevich Design Bureau)

The maximum speed of the MiG 17 is 1,145 kilometers per hour (711 miles per hour). The interceptor has a practical range 1,240 kilometers (770 miles) and practical ceiling of 16,600 meters (54,462 feet). For high altitude missions, pilots wore a Zvezda VSS-04 pressure suit.

The MiG 17 was originally armed with two Nudelman-Rikhter NR-23 23 mm autocannons with 80 rounds per gun, and a single, NR-37 37 mm autocannon, with 40 rounds of ammunition. Later, it could be armed with two NR30 30 mm autocannons with 70 rounds per gun. This gun used 30x155mm high explosive or armor piercing ammunition. It has a rate of fire of 900 rounds per minute.

More than 10,000 MiG 17 fighters were built in the Soviet Union, Poland and China. The type remains in service with North Korea.

© 2023, Bryan R. Swopes