Tag Archives: Mikoyan-Gurevich MiG 17

26 March 1967

Republic F-105D-6-RE Thunderchief 59-1772, parked in a revetment. Colonel Scott flew this airplane 26 March 1967 when he shot down a MiG-17. (U.S. Air Force)
Republic F-105D-6-RE Thunderchief 59-1772, parked in a revetment. Colonel Scott flew this airplane 26 March 1967 when he shot down a MiG 17. (U.S. Air Force)

26 March 1967: Colonel Robert Ray Scott, United States Air Force, commanding the 355th Tactical Fighter Wing, was leading 20 Republic F-105 Thunderchief fighter bombers from Takhli Royal Thai Air Force Base, Thailand, on an attack against an enemy military barracks near Hanoi, North Vietnam. Colonel Scott’s airplane was Republic F-105D-6-RE, serial number 59-1772, and his call sign was “Leech 01.” As he came off the target, he shot down an enemy Mikoyan-Gurevich MiG 17 fighter with the 20 mm M61A1 Vulcan cannon of his fighter bomber.

Colonel Robert R. Scott, U.S. Air Force
Colonel Robert R. Scott, U.S. Air Force

The third MiG-17 destroyed during the month was credited to the 355th TFW, Colonel Scott, who was leading an F-105 flight on a strike mission not far from Hoa Lac airfield on 26 March. His account follows:

“I had acquired the target and executed a dive-bomb run, while heading approximately 250°, altitude approximately 4,000 feet, I observed a MiG taking off from Hoa Loc airfield. I began a left turn to approximately 150° to follow the MiG for possible engagement. At this time I observed three more MiG-17s orbiting the airfield at approximately 3,000 feet, in single ship trail with 3,000 to 5,000 feet spacing. MiGs were silver with red star. I then concentrated my attention on the nearest MiG-17 and pressed the attack. As I closed in on the MiG it began turning to the right. I followed the MiG, turning inside, and began firing. I observed ordnance impacting on the left wing and pieces of material tearing off. At this time the MiG began a hard left-descending turn. I began to overshoot and pulled off high and to the right. The last time I saw the MiG it was extremely low, approximately 500 feet, and rolling nose down.”

Aces and Aerial Victories: The United States Air Force in Southeast Asia 1965–1973, by R. Frank Futrell, William H. Greenhalgh, Carl Grubb, Gerard E. Hasselwander, Robert F. Jakob and Charles A. Ravenstein, Office of Air Force History, Headquarters USAF, 1976, Chapter II at Page 45.

This former Egyptian Air Force Mikoyan-Gurevivch MiG-17F in the collection of the National Museum of the United States Air Force is painted in the colors of the Vietnam Peoples' Air Force. (U.S. Air Force)
This former Egyptian Air Force Mikoyan-Gurevivch MiG 17F in the collection of the National Museum of the United States Air Force is painted in the colors of the Vietnam Peoples’ Air Force. (U.S. Air Force)

The pilot of the MiG 17, Second Lieutenant Vũ Huy Lượng, 923rd Fighter Regiment, Vietnam Peoples’ Air Force, was killed.

As a Northrop P-61 Black Widow pilot with the 426th Night Fighter Squadron during World War II, Colonel Scott had shot down two enemy airplanes. By destroying the MiG-17, he became only the second U.S. Air Force pilot, after Colonel Robin Olds, to achieve aerial victories during World War II and the Vietnam War.

Mikoyan Gurevich MiG-17F in Vietnam Peoples' Air Force markings at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force).
Mikoyan-Gurevich MiG 17F in Vietnam Peoples’ Air Force markings at NMUSAF, Wright-Patterson AFB. (U.S. Air Force).

Robert Ray Scott was born at Des Moines, Iowa, 1 November 1920. He was the first of two children of Ray Scott, a railroad worker, and Elva M. Scott. He graduated from North High School in Des Moines, January 1939. He studied aeronautical engineering at the University of Iowa for two years before he enlisted as an Aviation Cadet in the U.S. Army Air Corps, 15 August 1941. Scott was 5 feet, 7 inches (1.70 meters) tall and weighed 144 pounds (65.3 kilograms). He was trained as a pilot and and was commissioned as a Second Lieutenant, 16 March 1942. He was assigned as an instructor pilot in California, and was promoted to 1st Lieutenant 15 December 1942.

Scott was transferred to the 426th Night Fighter Squadron, 14th Air Force, flying the Northrop P-61 Black Widow in India and China. He was promoted to captain, 3 May 1944, and to major, 16 August 1945. Major Scott was credited with shooting down two enemy aircraft. He was awarded the Distinguished Flying Cross and the Air Medal.

Captain Robert Ray Scott (back row, second from left) with the 426th Night Fighter Squadron, 1944. The airplane is a Northrop P-61 Black Widow. (U.S. Air Force)

Following World War II, Major Scott returned to the University of Iowa to complete his bachelor’s degree. He also earned two master’s degrees.

In 1952 he graduated from the Air Force test pilot school at Edwards Air Force Base, then served as a project pilot on the North American F-86D all-weather interceptor. Later he was a project officer at Edwards AFB on the Republic F-105 Thunderchief Mach 2 fighter-bomber.

Scott flew the North American Aviation F-86F Sabre during the Korean War. From January to July 1953, he flew 117 combat missions. From 1953 to 1956, Lieutenant Colonel Scott commanded the 405th Fighter Bomber Wing, Tactical Air Command, at Langley Air Force base, Virginia.

Lieutenant Richard Hill and Lieutenant Colonel Robert R. Scott (in cockpit) after their record-breaking transcontinental flight. (Unattributed)

On 9 October 1955, Scott set a transcontinental speed record by flying a Republic F-84F Thunderstreak fighter bomber from Los Angeles International Airport, California, to Floyd Bennett Field, New York, in 3 hours, 46 minutes, 33.6 seconds. Later he was a project officer at Edwards AFB on the Republic F-105 Thunderchief Mach 2 fighter-bomber.

Scott was promoted the rank of Colonel in 1960.

During the Vietnam War, Colonel Scott commanded the 355th Tactical Fighter Wing, flying 134 combat missions in the Republic F-105 Thunderchief.

Colonel Scott’s final commanding was the 832nd Air Division, 12th Air Force, at Cannon Air Force Base, New Mexico. He retired 1 September 1970 after 29 years of military service.

Colonel Robert Ray Scott flew 305 combat missions in three wars. During his Air Force career, Colonel Scott was awarded four Silver Star medals, three Legion of Merit medals, six Distinguished Flying Crosses and 16 Air Medals. He died at Tehachapi, California, 3 October 2006 at the age of 86 years. He is buried at the Arlington National Cemetery.

Republic F-105D 59-1772 is credited with another air-to-air victory. Just over a month after Colonel Scott’s Mig-17 shoot-down, on 28 April 1967 Major Harry E. Higgins, 357th Tactical Fighter Squadron, shot down another MiG-17 with the fighter bomber’s cannon, for which Major Higgins was awarded the Silver Star.

The Thunderchief, though, met its own end when it was shot down by 37 mm anti-aircraft gunfire 10 miles (16 kilometers) west of Ko Hinh, Laos, 27 January 1970. The pilot was rescued.

Colonel Robert R. Scott, commander, 355th Tactical Fighter Wing, checks the bombs loaded on a multiple ejector rack while preflighting his Republic F-105 Thunderchief. (U.S. Air Force)
Colonel Robert R. Scott, commander, 355th Tactical Fighter Wing, checks the bombs loaded on a multiple ejector rack while preflighting his Republic F-105 Thunderchief. (U.S. Air Force)

The F-105 was the largest single-seat, single-engine combat aircraft in history. It was designed as a Mach 2+ tactical nuclear strike aircraft and fighter-bomber. Republic Aviation Corporation built 833 F-105 Thunderchief fighter bombers at its Farmingdale, New York factory. 610 of those were single-seat F-105Ds.

The F-105D Thunderchief is 64 feet, 5.3 inches (19.642 meters) long with a wingspan of 34 feet, 11.2 inches (10.648 meters) and overall height of 19 feet, 8.4 inches (6.005 meters). The total wing area was 385 square feet (35.8 square meters). Its wings were swept 45° at 25% chord. The angle of incidence was 0° and there was no twist. The wings had 3° 30′ anhedral. The F-105D-31 has an empty weight of 26,855 pounds (12,181 kilograms) and a maximum takeoff weight of 52,838 pounds (23,967 kilograms).

This Republic F-105D-10-RE Thunderchief, 60-0504, served with the 355th TFW at Takhli AB, Thailand. It shot down two enemy fighters. Similar the the F-105D flown by Colonel Scott, 26 March 1967, it is in the collection of the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio. (U.S. Air Force)

The Thunderchief was powered by one Pratt & Whitney J75-P-19W engine. The J75 is a two-spool axial-flow afterburning turbojet with water injection. It has a 15-stage compressor section (8 low- and and 7 high-pressure stages) and 3-stage turbine section (1 high- and 2 low-pressure stages.) The J75-P-19W is rated at 14,300 pounds of thrust (63.61 kilonewtons), continuous power; 16,100 pounds (71.62 kilonewtons), Military Power (30-minute limit); and Maximum Power rating of 24,500 pounds (108.98 kilonewtons) with afterburner (15-minute limit). The engine could produce 26,500 pounds of thrust (117.88 kilonewtons) with water injection, for takeoff. The J75-P-19W is 21 feet, 7.3 inches (6.586 meters) long, 3 feet, 7.0 inches (1.092 meters) in diameter, and weighs 5,960 pounds (2,703 kilograms).

Republic F-105D Thunderchief 60-0504 at the National Museum of the United States Air Force. (U.S. Air Force)

The maximum speed of the F-105D was 726 knots (835 miles per hour/1,345 kilometers per hour) at Sea Level (Mach 1.09) and 1,192 knots (1,372 miles per hour (2,208 kilometers per hour) at 36,089 feet (11,000 meters) (Mach 2.08). The combat ceiling was 51,000 feet (15,545 meters). The F-105D’s combat radius varied with the type of mission from 277 to 776 nautical miles (319–893 statute miles/513–1,437 kilometers). The maximum ferry range was 1,917 nautical miles (2,206 statute miles/3,550 kilometers).

The F-105D was armed with one 20 mm M61A1 Vulcan rotary cannon and 1,028 rounds of ammunition. It has an internal bomb bay and can carry bombs, missiles or fuel tanks on under wing and centerline hardpoints. The maximum bomb load consisted of 16 750-pound (340 kilogram) bombs. For tactical nuclear strikes, the F-105D could carry one B57 or three B61 nuclear bombs.

Two Air Force sergeants load belts of linked 20-millimeter cannon shells for the F-105’s M61 six-barreled Gatling gun. (U.S. Air Force)

The F-105 Thunderchief was a supersonic tactical fighter bomber rather than an air superiority fighter. Still, during the Vietnam War, F-105s shot down 27 enemy MiG fighters. 24 of those were shot down with the Thunderchief’s Vulcan cannon.

Of the 833 F-105s, 395 were lost during the Vietnam War. 334 were shot down, mostly by antiaircraft guns or missiles, and 17 by enemy fighters. Another 61 were lost due to accidents. The 40% combat loss is indicative of the extreme danger of the missions these airplanes were engaged in.

Republic F-105D Thunderchief at Takhli TRAFB. (U.S. Air Force)

© 2021, Bryan R. Swopes

10 March 1967

Republic F-105D-31-RE Thunderchief 62-4284 was a triple MiG killer. Captain Max C. Brestel shot down two MiG-17 fighters with this airplane, 10 March 1967. Captain Gene I. Basel also shot down a MiG-17 while flying this fighter bomber, 27 October 1967.
Republic F-105D-31-RE Thunderchief 62-4284 was a triple MiG killer. Captain Max C. Brestel shot down two MiG-17 fighters with this airplane, 10 March 1967. Captain Gene I. Basel also shot down a MiG-17 while flying this fighter bomber, 27 October 1967. (U.S. Air Force)

10 March 1967: Captain Max C. Brestel, United States Air Force, a pilot assigned to the 354th Tactical Fighter Squadron, 355th Tactical Fighter Wing at Takhli Royal Thai Air Force Base, was flying a Republic F-105D-31-RE Thunderchief fighter-bomber, serial number 62-4284. His call sign was “Kangaroo 03.” During an attack on the Thai Nguyen Steel Mill, the single most heavily-defended target in North Vietnam, Captain Brestel engaged and shot down two enemy MiG-17 fighters.

This was the first time during the Vietnam War that an American pilot shot down two enemy airplanes during the same mission. The following description is from an official U.S. Air Force history:

Brestel’s aerial victories became the first USAF double kill of the conflict. At the time, he was flying the third Thunderchief in a flight of four and was tasked with suppressing flak in and around the Thai Nguyen steel mill and supporting other F-105 strike forces. Brestel relates how his two victories came about:

“We proceeded to the target via the Red River to a point north of the target, where we turned south. Numerous SAM and MiG warnings had been transmitted. Also, the 388th Wing, which had preceded us on the target, had encountered MiGs.

“As the flight pulled up to gain altitude for delivering our ordnance, I sighted two MiG-21s making a pass at Col. Gast [Lt. Col. Philip C. Gast, the flight leader] from his 4 o’clock position. I was in lead’s 8:30 o’clock position. I broke toward the MiGs and passed across his tail. They broke off the attack and I continued on my dive delivery. Flak was normal for the area. We delivered our ordnance as planned.”

As the flight pulled out at an altitude of approximately 3,000 to 4,000 feet, Gast called MiGs at 2 o’clock low. ‘Let’s go get them,’ he urged. ‘I’m with you,’ Brestel acknowledged as he spotted the flight of four MiG-17s in staggered trail heading north at approximately 1,500 feet. Behind them was another flight of four. Brestel’s narrative continues:

“I observed all MiGs light their afterburners. Colonel Gast began firing at one of the first two MiGs. I observed the second two begin to fire at Colonel Gast. I called a break and closed within 300–500 feet of the number four MiG. I fired an approximate 2½ second burst at him as he was in a right turn. I observed hits in the wing and fuselage. The MiG reversed into a left turn. I fired another 2½ second burst into him, observing hits in the left wing, fuselage and canopy, and a fire in the left wing root. The aircraft rolled over and hit the ground under my left wing. I then closed 300 feet on the number three MiG, which was firing at Colonel Gast. He was in a right turn and again I fired a 2½ second burst, observing hits in wing, fuselage, etc. He also reversed to the left and I fired another 2½ second burst, observing more hits and pieces flying off the aircraft. The aircraft appeared to flip back up over my canopy and disappeared behind me. we broke off the engagement at this time after approximately 1½ to 2 minutes of combat. A SAM was fired at us and more flak as we exited the area.

“I know I destroyed the first MiG, as I saw him crash. I did not see the pilot bail out and doubt if he was alive, since hits were observed in the cockpit and the canopy broke up. My wingman, Lt. Weskamp [1st Lt. Robert L. Weskamp] also observed the MiG hit the ground.

“I feel I also destroyed the second MiG, as the range was the same and hits were observed in the same areas, i.e., fuselage, wings, etc. Also, his last maneuver could not be considered normal. The aircraft appeared to be in a violent pitch-up or tumble and out of control… However, because he pitched up over and behind me, I did not see him strike the ground.”

Brestel was given credit for destroying both MiGs.

— Aces and Aerial Victories: The United States Air Force in Southeast Asia 1965–1973, by R. Frank Futrell, William H. Greenhalgh, Carl Grubb, Gerard E. Hasselwander, Robert F. Jakob and Charles A. Ravenstein, Office of Air Force History, Headquarters USAF, 1976, Chapter II at Pages 44 and 45.

This former Egyptian Air Force Mikoyan-Gurevivch MiG-17F in the collection of the National Museum of the United States Air Force is painted in the colors of the Vietnam Peoples' Air Force. (U.S. Air Force)
This former Egyptian Air Force Mikoyan-Gurevivch MiG-17F in the collection of the National Museum of the United States Air Force is painted in the colors of the Vietnam Peoples’ Air Force. (U.S. Air Force)

Vietnamese sources identified one of the downed MiG-17 fighters as being of Z Group, Korean People’s Air Force, flown by Kim Quang Wook, who was killed.

The F-105 was the largest single-seat, single-engine combat aircraft in history. It was designed as a Mach 2+ tactical nuclear strike aircraft and fighter-bomber. The fuselage of the F-105B incorporated the “area rule” which gave the Thunderchief its characteristic “wasp waist” shape.

The F-105D Thunderchief is 64 feet, 5.3 inches (19.642 meters) long with a wingspan of 34 feet, 11.2 inches (10.648 meters) and overall height of 19 feet, 8.4 inches (6.005 meters). The total wing area was 385 square feet (35.8 square meters). Its wings were swept 45° at 25% chord. The angle of incidence was 0° and there was no twist. The wings had 3° 30′ anhedral. The F-105D-31 has an empty weight of 26,855 pounds (12,181 kilograms) and a maximum takeoff weight of 52,838 pounds (23,967 kilograms).

The Thunderchief was powered by one Pratt & Whitney J75-P-19W engine. The J75 is a two-spool axial-flow afterburning turbojet with water injection. It has a 15-stage compressor section (8 low- and and 7 high-pressure stages) and 3-stage turbine section (1 high- and 2 low-pressure stages.) The J75-P-19W is rated at 14,300 pounds of thrust (63.61 kilonewtons), continuous power; 16,100 pounds (71.62 kilonewtons), Military Power (30-minute limit); and Maximum Power rating of 24,500 pounds (108.98 kilonewtons) with afterburner (15-minute limit). The engine could produce 26,500 pounds of thrust (117.88 kilonewtons) with water injection, for takeoff. The J75-P-19W is 21 feet, 7.3 inches (6.586 meters) long, 3 feet, 7.0 inches (1.092 meters) in diameter, and weighs 5,960 pounds (2,703 kilograms).

The maximum speed of the F-105D was 726 knots (835 miles per hour/1,345 kilometers per hour) at Sea Level (Mach 1.09) and 1,192 knots (1,372 miles per hour (2,208 kilometers per hour) at 36,089 feet (11,000 meters) (Mach 2.08). The combat ceiling was 51,000 feet (15,545 meters). The F-105D’s combat radius varied with the type of mission from 277 to 776 nautical miles (319–893 statute miles/513–1,437 kilometers). The maximum ferry range was 1,917 nautical miles (2,206 statute miles/3,550 kilometers).

The F-105D was armed with one 20 mm M61A1 Vulcan rotary cannon and 1,028 rounds of ammunition. It has an internal bomb bay and can carry bombs, missiles or fuel tanks on under wing and centerline hardpoints. The maximum bomb load consisted of 16 750-pound (340 kilogram) bombs. For tactical nuclear strikes, the F-105D could carry one B57 or three B61 nuclear bombs.

The F-105 Thunderchief was a supersonic tactical fighter bomber rather than an air superiority fighter. Still, during the Vietnam War, F-105s shot down 27 enemy MiG fighters. 24 of those were shot down with the Thunderchief’s Vulcan cannon.

Two Air Force sergeants load belts of linked 20-millimeter cannon shells for the F-105's M61 six-barreled Gatling gun. (U.S. Air Force)
Two Air Force sergeants load belts of linked 20-millimeter cannon shells for the F-105’s M61 six-barreled Gatling gun. (U.S. Air Force)

Republic Aviation Corporation built 833 F-105 Thunderchief fighter bombers at its Farmingdale, New York factory. 610 of those were single-seat F-105Ds. Of the 833 F-105s, 395 were lost during the Vietnam War. 334 were shot down, mostly by antiaircraft guns or missiles, and 17 by enemy fighters. Another 61 were lost due to accidents. The 40% combat loss is indicative of the extreme danger of the missions these airplanes were engaged in.

62-4284 is the only F-105 Thunderchief officially credited with shooting down three enemy fighters during the Vietnam War. Flown by Captain Gene I. Basel, also of the 354th Tactical Fighter Squadron, 62-4284 was “Bison 02” on an attack against the Canal de Rapides Bridge, 27 October 1967. Captain Basel shot down a MiG-17 with the Thunderchief’s 20 mm cannon. The VPAF pilot ejected.

Having survived the Vietnam War, 62-4284 crashed during a peacetime training mission, 4 miles south west of Clayton, Oklahoma, 12 March 1976. The pilot, Captain Larry L. Kline, 465th Tactical Fighter Squadron, Hill Air Force Base, Utah, was killed.

Republic F-105D-31-RE Thunderchief 62-4347, 333d TFS, Takhli RTAFB, circa 1966. This is the same type aircraft as 62-4284. (U.S. Air Force)

© 2021, Bryan R. Swopes

14 January 1950

This is the second Mikoyan Gurevich I 330 prototype, SI 02.
This is the second Mikoyan Gurevich I 330 prototype, SI 02.

14 January 1950: The Mikoyan Gurevich prototype fighter I 330 SI made its first flight with test pilot Ivan Ivashchenko. It would be developed into the MiG 17.

The MiG 17 was an improved version of the earlier MiG 15. It was a single-seat, single engine fighter armed with cannon, and capable of high subsonic and transonic speed.

Mikoyan Gurevich MiG 17.
Mikoyan Gurevich MiG 17.

The prototype’s wings were very thin and this allowed them to flex. The aircraft suffered from “aileron reversal,” in that the forces created by applying aileron to roll the aircraft about its longitudinal axis were sufficient to bend the wings and that caused the airplane to roll in the opposite direction.

The first prototype I 330 SI developed “flutter” while on a test flight, 17 March 1950. This was a common problem during the era, as designers and engineers learned how to build an airplane that could smoothly transition through the “sound barrier.” The rapidly changing aerodynamic forces caused the structure to fail and the horizontal tail surfaces were torn off. The prototype went into an unrecoverable spin. Test pilot Ivashchenko was killed.

Two more prototypes, SI 02 and SI 03, were built. The aircraft was approved for production in 1951.

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

A MiG 17 in flight.
A MiG 17 in flight.
Иван Т. Иващенко летчик-испытатель
Иван Т. Иващенко летчик-испытатель

Ива́н Тимофе́евич Ива́щенко (Ivan T. Ivashchenko) was born at Ust-Labinsk, Krasnodar Krai, Russia, 16 October 1905. He served in the Red Army from 1927 to 1930. He graduated from the Kuban State University in 1932.

Ivashchenko was trained as a pilot at the Lugansk Military Aviation School at Voroshilovgrad, and a year later graduated from the Kachin Military Aviation College at Volgograd.

In 1939, he fought in The Winter War. During the Great Patriotic War, Ivan Ivashchenko flew with a fighter squadron in the defense of Moscow.

From 1940 to 1945, Ivan Ivashchenko was a test pilot. He trained at the M.M. Gromov Flight Research Institute at Zhokovsky, southeast of Moscow, in 1941. He was assigned to Aircraft Factory No. 18 at Kuibyshev (Samara) from 1941 to 1943. Ivashchenko flew the Ilyushin Il-2 Sturmovik fighter bomber extensively. From 1943 to 1945 he was a test pilot for Lavochkin OKB at Factory 301 in Khimki, northwest of Moscow.

In 1945 Ivashchenko was reassigned to OKB Mikoyan, where he worked on the development of the MiG 15 and MiG 17 fighters. He participated in testing ejection seat systems and in supersonic flight.

Ivan T. Ivashchenko was a Hero of the Soviet Union, and was awarded the Order of Lenin, Order of the Red Banner (two awards) and Order of the Patriotic War. Killed in the MiG 17 crash at the age of 44 years, he was buried at the Novodevichy Cemetery in Moscow.

© 2017, Bryan R. Swopes

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 Semipaltinsk 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

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

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

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