Tag Archives: Fighter Bomber

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

9 March 1955

Col. Robert R. Scott waves from the cockpit of his Republic F-84F Thunderstreak after completing a record-breaking transcontinental flight, 9 March 1955. (AP Photo)
Lieutenant Richard Hill and Lieutenant Colonel Robert R. Scott (in cockpit) after their record-breaking transcontinental flight. (Unattributed)

9 March 1955: Lieutenant Colonel Robert Ray Scott, United States Air Force, commanding officer, 510th Fighter Bomber Squadron, 405th Fighter Bomber Wing, Langley Air Force Base, Virginia, with Major Robert C. Ruby and Captain Charles T. Hudson, flew their Republic F-84F Thunderstreaks non-stop from Los Angeles Airport (LAX), on the southern California coastline, to overhead Floyd Bennett Field, New York. Two in-flight refuelings from Boeing KB-29 tankers were required.

Colonel Scott’s flight set a new National Aeronautic Association speed record with an elapsed time of 3 hours, 44 minutes, 53.88 seconds.

A newspaper article from the following day describes the event:

2 Des Moines Pilots Break Speed Record

NEW YORK (AP) — Two air force pilots from Des Moines broke the speed record from Los Angeles to New York Wednesday, making a nonstop flight in less than four hours.

Lt. Col. Robert R. Scott, 34, flying a Republic F-84F Thunderstreak jet fighter, turned in the fastest time — 3 hours 46 minutes and 33 seconds. He averaged 649 miles an hour.

Just one minute behind was another Des Moines pilot, Maj. Robert C. Ruby, 32. His time was 3:47:33.

The old mark for the 2,445-mile route was 4:06:16, set Jan 2, 1954, by an air national guard pilot.

Refueling Slow

The pilots said they could have made faster time except for slow and obsolete in-flight refueling tanker planes.

A third pilot who shattered the old mark is Capt. Charles T. Hudson, 33, of Gulfport, Miss., who made the flight in 3:49:53.

Eight air force Thunderstreaks left Los Angeles in a mass assault on the record. Five dropped out through failure to make contact with refueling planes or other reasons. All reportedly landed safely.

While setting a Los Angeles–New York record, Scott failed to beat the navy’s time from San Diego, Calif., to New York — 2,438 miles, or seven miles shorter than Wednesday’s flight.

Flew Cougar Jet

Lt. Comdr. Francis X. Brady, 33, of Virginia Beach, Va., flew from San Diego in 3:45:30 on April 1, 1954, flying a Grumman F9F Cougar.

The air force planes flew at about 40,000 feet.

“The tankers used for refueling are much too obsolete and too old,” Scott commented on landing.

The jets had to slow to 200 m.p.h. from almost 650 to take on fuel.

Scott said he refueled twice — once near La Junta, Colo., and once near Rantoul, Ill.

Others Agree

Ruby and Hudson also said they could have made faster time if the tank planes were more modern.

Hudson and Ruby carried extra gas tanks and made one in-flight refueling each. Scott carried no extra gas and had two in-flight refuelings.

1st Lt. James E. Colson of Middleboro, Ky., tried to make it with no refueling. He got as far as Pittsburgh, Pa.

Of the other four unable to complete the flight, one dropped out in California, two in Kansas and one at Sedalia, Mo.

The Daily Iowan, Thursday, March 10, 1955, Page 1, Column 1

Cockpit of Republic F-84F-10-RE Thunderstreak 51-1405. (U.S. Air Force)
Lieutenant Colonel Robert R. Scott, U.S. Air Force, 5 March 1955. (U.S. Air Force photograph)
Lieutenant Colonel Robert R. Scott, U.S. Air Force, 5 March 1955. (U.S. Air Force photograph)

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, 14th Air Force, Chengdu, China 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.

Scott was promoted to the rank of Colonel in 1960.

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)

During the Vietnam War, Colonel Scott commanded the 355th Tactical Fighter Wing, flying 134 combat missions in the Republic F-105 Thunderchief. On 26 March 1967 he shot down an enemy MiG-17 fighter near Hanoi with the 20 mm M61 Vulcan cannon of his F-105D-6-RE, 59-1772, making him only the second Air Force pilot with air combat victories in both World War II and Vietnam.

Colonel Scott’s final command 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-84F-1-RE Thunderstreak 51-1346. (U.S. Air Force)

The Republic F-84F Thunderstreak was an improved, swept-wing version of the straight-wing F-84 Thunderjet fighter bomber. The first production Thunderstreak, 51-1346, flew for the first time, 22 May 1952, with company test pilot Russell M. (Rusty”) Roth in the cockpit.

The F-84F was 43 feet, 4¾ inches (13.227 meters) long with a wingspan of 33 feet, 7¼ inches (10.243 meters) and overall height of 14 feet, 4¾ inches (4.388 meters). The wings were swept aft 40° at 25% chord. Their angle of incidence was 1° 30′ and there was no twist. The F-84F had 3° 30′ anhedral. The Thunderstreak had an empty weight if 13,645 pounds (6,189 kilograms) and maximum takeoff weight of 27,000 pounds (12,247 kilograms).

The initial F-84F-1-RE aircraft were powered by a Wright J65-W-1 turbojet, a license-built variant of the British Armstrong Siddely Sapphire. Later versions used Wright J65-W-3 and J65-W-7, or Buick J65-B-3 or J65-B-7 engines. The J65-B-3 was a single-shaft axial-flow turbojet with a 13-stage compressor section and 2-stage turbine. The W-3/B-3 had a continuous power rating of 6,350 pounds of thrust (28.25 kilonewtons) at 8,000 r.p.m. It produced 7,220 pounds of thrust (32.12 kilonewtons) at 8,300 r.p.m. (5-minute limit). The J65-B-3 was 10 feet, 8.6 inches (3.266 meters) long, 3 feet, 1.7 inches (0.958 meters) in diameter, and weighed 2,785 pounds (1,263 kilograms).

Republic F-84F-1-RE Thunderstreak 51-1346, the first production airplane, at Farmingdale, New York, 1952. (Republic Aviation Corporation)

The F-84F had a maximum speed of 595 knots (685 miles per hour/1,102 kilometers per hour) at Sea Level (0.900 Mach). The fighter bomber could climb at 7,000 feet per minute (36 meters per second). Its service ceiling was 44,450 feet (13,548 meters). The fighter bomber’s maximum ferry range was 2,010 nautical miles (2,313 statute miles/3,723 kilometers).

Armament consisted of six Browning .50-caliber (12.7 × 99 NATO) AN-M3 aircraft machine guns, with two mounted in the wing roots and four in the nose. The were 300 rounds of ammunition per gun. Up to 6,000 pounds (2,722 kilograms) of bombs and rockets could be carried under the wings. A variable-yield Mark 7 tactical nuclear weapon could also be carried.

Between 1952 and 1957, 2,112 F-84F Thunderstreaks were built by Republic at Farmingdale, New York, and by General Motors at Kansas City, Kansas. The Thunderstreak served with the United States Air Force and Air National Guard until 1971.

Republic F-84F-5-RE Thunderstreak 51-1366. (Republic Aviation Corporation)
First Lieutenant Richard Bach, U.S. Air Force, in the cockpit of a Republic F-84F-35-RE Thunderstreak, 52-6490, at Chaumont Air Base, France, 1962. Richard Bach is the author of the classic aviation novel, “Stranger to the Ground.” (Jet Pilot Overseas)

© 2019, Bryan R. Swopes

28 February 1946

Republic XP-84 Thunderjet 45-59475 takes of at Muroc AAF, California. (U.S. Air Force )
Republic XP-84 prototype 45-59475 at landing at Muroc Army Airfield, California, 1946. (U.S. Air Force )
Wallace A. Lien

28 February 1946: At Muroc Army Airfield, California, (now, Edwards Air Force Base) the first of three prototype Republic Aviation Corporation  XP-84 Thunderjet fighter bombers, serial number 45-59475, made its first flight with company test pilot Wallace Addison Lien in the cockpit.

Alexander Kartveli, Chief Engineer of the Republic Aviation Corporation, began working on the XP-84 during 1944 as a jet-powered successor to the company’s P-47 Thunderbolt fighter bomber. The prototype was completed at the factory in Farmingdale, New York, in December 1945. It was then partially disassembled and loaded aboard Boeing’s prototype XC-97 Stratofreighter and flown west to Muroc Army Airfield in the high desert of southern California. It was reassembled and prepared for its first flight.

The prototype Republic XP-84, as yet unpainted. (San Diego Air & Space Museum Archive)

The XP-84 was 37 feet, 2 inches (11.328 meters) long, with a wingspan of 36 feet, 5 inches (11.100 meters) and overall height of 12 feet, 10 inches (3.912 meters). The wings had a total area of 260 square feet ( square meters). The leading edges were swept aft to 6° 15′. The angle of incidence was 0° with -2° of twist and 4° dihedral. The airplane had an empty weight of 9,080 pounds (4,119 kilograms) and gross weight of 13,400 pounds (6,078 kilograms).

Republic XP-84. (U.S. Air Force photo)

The XP-84 was powered by a General Electric J35-GE-7 engine. The J35 was a single-spool, axial-flow turbojet engine with an 11-stage compressor and single-stage turbine. The J35-GE-7 was rated at 3,750 pounds of thrust (16.68 kilonewtons) at 7,700 r.p.m. (5-minute limit). The engine was 14 feet, 0.0 inches (4.267 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,400 pounds (1,089 kilograms).

The first of three prototypes, Republic XP-84 Thunderjet 45-59475 is parked on the dry lake at Muroc Army Airfield. (U.S. Air Force)
The first of three prototypes, Republic XP-84 Thunderjet 45-59475 is parked on the dry lake at Muroc Army Airfield. (U.S. Air Force)

The XP-84 had a cruise speed of 440 miles per hour (708 kilometers per hour) and maximum speed of 592 miles per hour (953 kilometers per hour). The service ceiling was 35,000 feet (10,668 meters), which it could reach in approximately 13 minutes. The maximum range was 1,300 miles (2,092 kilometers).

Republic XP-84 Thunderjet. (U.S. Air Force)
Republic XP-84 Thunderjet 45-59475. (U.S. Air Force)
Republic XP-84 Thunderjet (U.S. Air Force)
Republic XP-84 Thunderjet 45-59475. (U.S. Air Force)
Republic XP-84 Thunderjet (U.S. Air Force)
Republic XP-84 Thunderjet 45-59475. (U.S. Air Force)
Republic XP-84 Thunderjet (U.S. Air Force)
Republic XP-84 Thunderjet 45-59475. (U.S. Air Force)
Republic XP-84 Thunderjet 45-59475 in flight. (U.S. Air Force)
Republic XP-84 Thunderjet 45-59475 in flight. (U.S. Air Force)

Wallace Addison Lien was born at Alkabo, in Divide County, at the extreme northwest corner of North Dakota, 13 August 1915. He was the second of six children of Olaf Paulson Lien, a Norwegian immigrant and well contractor, and Elma Laura Richardson Lien.

Wallace A. Lien (The 1939 Gopher)

Wally Lien graduated from the University of Minnesota Institute of Technology 17 June 1939 with a Bachelor’s Degree in Mechanical Engineering (B.M.E.). He was a president of the Pi Tau Sigma (ΠΤΣ) fraternity, a member of the university’s cooperative book store board, and a member of the American Society of Mechanical Engineers (A.S.M.E.). He later studied at the California Institute of Technology (CalTech) at Pasadena, California, and earned a master’s degree in aeronautical engineering.

Lien worked as a an engineer at a steel sheet mill in Pennsylvania. He enlisted in the  the United States Army at Pittsburgh, Pennsylvania, 18 February 1941. He was accepted as an aviation cadet at Will Rogers Field, Oklahoma City, Oklahoma, 11 November 1941. 26 years old, Lien was 6 feet, 2 inches (1.88 meters) tall and weighed 174 pounds (79 kilograms). During World War II, Lien remained in the United States, where he served as a test pilot at Wright Field, Dayton, Ohio. He conducted flight tests of the Bell YP-59A Airacomet and the Lockheed XP-80 Shooting Star. Having reached the rank of Major, he left the Air Corps, 16 February 1946. Lien then worked for the Republic Aviation Corporation, testing the XP-84. A few months later, Lien went to North American Aviation, where he made the first flight of the the XFJ-1 Fury, 11 September 1946

Wally Lien married Miss Idella Muir at Elizabeth, New Jersey, 26 December 1946. They would have two children.

Wallace Addison Lien died at Colorado Springs, Colorado, 28 October 1994, at the age of 79 years. He was buried at the Shrine of Remembrance Veterans Honor Court, Colorado Springs, Colorado

© 2019, Bryan R. Swopes

23 February 1951

Dassault Mystere 01, F-FWUU
Dassault Mystère MD.452, F-WFUU. (Dassault Aviation)
Constantin Wladimir Rozanoff. (Dassault)
Konstantin Wladimir Rozanoff. (Dassault Aviation)

23 February 1951: At Istres, France, Société des Avions Marcel Dassault chief test pilot Konstantin Wladimir (“Kostia”) Rozanoff made the first flight of the Mystère MD.452 prototype, F-WFUU, c/n 01. This was a development of the Dassault Ouragan MD.450 with the wings’ leading edge swept from 14° to 30°. It was powered by a Rolls-Royce Nene turbojet engine. Rozanoff believed, though it was not confirmed, that he had broken the Sound Barrier.

A series of prototypes were built before the fighter bomber was put into production as the Mystère IIC. 171 were built between 1954 and 1957.

Kostia Romanoff with the first prototype Dassault Mystere. (Dassault)
Kostia Rozanoff with the first prototype Dassault Mystère, F-WFUU, c/n 01. (Dassault Aviation)

The Mystère IIC was a single seat, single engine turbojet-powered fighter bomber produced for the Armée de l’Air. It was 38 feet 6 inches (11.735 meters) long with a wingspan of 42 feet, 9 inches (13.030 meters) and overall height of 14 feet (4.267 meters). The fighter had an empty weight of 11,495 pounds (5,214 kilograms) and maximum takeoff weight of 16,480 pounds (7,475 kilograms). The powerplant was a SNECMA ATAR 101D-1 turbojet which produced 6,610 pounds of thrust (29.403 kilonewtons).

The maximum speed of the Mystère IIC was 660 miles per hour (1,062 kilometers per hour). Its range was 550 miles (885 kilometers) and the service ceiling was 50,000 feet (15,240 meters).

Dassault Mystère MD.452, F-WFUU. (Dassault Aviation)
Dassault Mystère MD.452, F-WFUU. (Dassault Aviation)

The MD.452 was armed with two Direction des Études et Fabrications d’Armement (DEFA) 30mm revolver cannon with 150 rounds of ammunition per gun, and up to 2,000 pounds (907 kilograms) of bombs.

The prototype Dassault Mystère, F-WFUU, crashed at Istres 3 March 1953 when a wing tip fuel tank broke away and struck the airplane’s tail, killing test pilot Charles Monier.

Kostia Romanoff was killed 3 April 1954 while demonstrating a Mystère IVB.

Constantin Wladimir Rozanoff, Chief Pilot, Dassault Aviation, with a Mystère IV. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Konstantin Wladimir Rozanoff, Chief Pilot, Dassault Aviation, with a Mystère IV. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

© 2017, Bryan R. Swopes

13 January 2012

F-15E-47-MC Strike Eagle 89-0487 at Bagram Airfield, Afghanistan, 13 January 2012. (Photograph by Airman 1st Class Ericka Engblom, USAF)
McDonnell Douglas F-15E-47-MC Strike Eagle 89-0487, assigned to the 335th Expeditionary Fighter Squadron, taxis into its revetment at Bagram Airfield, Afghanistan, 13 January 2012. Note the World War II Eagle Squadron insignia and the green star kill mark painted on the fighter bomber’s nose. (Photograph by Airman 1st Class Ericka Engblom, USAF)

13 January 2012: This McDonnell Douglas F-15E-47-MC Strike Eagle, 89-0487, became the first F-15 to have logged over 10,000 flight hours. Regularly assigned to Captain Justin Pavoni, Pilot, and Lieutenant Colonel David Moeller, Weapons System Officer and commander of the 335th Expeditionary Fighter Squadron, on the mission which achieved the milestone, 487 was flown by Captain Ryan Bodenheimer, pilot, and Captain Erin Short, WSO, the two youngest flyers in the squadron.

89-0487 was accepted by the Air Force on 13 November 1990. At the time of this event, 487 was considered to be the flag ship of the 335th Expeditionary Fighter Squadron. During a three month period at Bagram Air Base, this individual F-15E flew 1,200 hours and dropped 15% of all the bombs dropped by the squadron.

During Operation Desert Storm, Captains Tim Bennett and Dan Bakke, USAF, flying this F-15E, call sign “Packard 41,” used a GBU-10 Paveway II 2,000-pound laser-guided bomb to “shoot down” an Iraqi Mi-24 Hind attack helicopter. 487 is the only F-15E to have scored an air-to-air victory.

This airplane is still in service with the United States Air Force. It passed 12,000 flight hours on 16 August 2016. It has been deployed for combat operations 17 times.

McDonnell Douglas F-15E Strike Eagle 89-0487 lands at Bagram Air Base after passing its 10,000th flight hour, 13 January 2012. (Airman 1st Class Ericka Engblom, U.S. Air Force)
With Captains Bodenheimer and Short in the cockpit, McDonnell Douglas F-15E-47-MC Strike Eagle 89-0487 lands at Bagram Airfield, Afghanistan, after passing its 10,000th flight hour, 13 January 2012. (Airman 1st Class Ericka Engblom, U.S. Air Force)

The Strike Eagle was begun as a private venture by McDonnell Douglas. Designed to be operated by a pilot and a weapons system officer (WSO), the airplane can carry bombs, missiles and guns for a ground attack role, while maintaining its capability as an air superiority fighter. It’s airframe was a strengthened and its service life doubled to 16,000 flight hours. The Strike Eagle became an Air Force project in March 1981, and  went into production as the F-15E. The first production model, 86-0183, made its first flight 11 December 1986.

Capt. Ryan Bodenheimer celebrates as he and Capt. Erin Short taxi onto the runway in F-15E Strike Eagle #89-0487 before the mission that will bring its logged flying hours up to 10,000. (U.S. Air Force photo/ Airman 1st Class Ericka Engblom)

The McDonnell Douglas F-15E Strike Eagle is a two-place twin-engine multi-role fighter. It is 63 feet, 9 inches (19.431 meters) long with a wingspan of 42 feet, 9¾ inches (13.049 meters) and height of 18 feet, 5½ inches (5.626 meters). It weighs 31,700 pounds (14,379 kilograms) empty and has a maximum takeoff weight of 81,000 pounds (36,741 kilograms). The F-15E is powered by two Pratt and Whitney F100-PW-229 turbofan engines which produce 17,800 pounds of thrust (79.178 kilonewtons) each, or 29,100 pounds (129.443 kilonewtons) with afterburner.

Captain Ryan Bodenheimer climbs down from the cockpit of F-15E Strike Eagle 89-0487 after completing the mission in which the aircraft passed the 10,000 flight hour mark. (U.S. Air Force)

The Strike Eagle has a maximum speed of Mach 2.54 (1,676 miles per hour, (2,697 kilometers per hour) at 40,000 feet (12,192 meters) and is capable of sustained speed at Mach 2.3 (1,520 miles per hour, 2,446 kilometers per hour). Its service ceiling is 60,000 feet (18,288 meters). The fighter-bomber has a combat radius of 790 miles (1,271 kilometers) and a maximum ferry range of 2,765 miles (4,450 kilometers).

Though optimized as a fighter-bomber, the F-15E Strike Eagle retains an air-to-air combat capability. The F-15E is armed with one 20mm M61A1 Vulcan 6-barrel rotary cannon with 512 rounds of ammunition, and can carry four AIM-9M Sidewinder heat-seeking missiles and four AIM-7M Sparrow radar-guided missiles, or a combination of Sidewinders, Sparrows and AIM-120 AMRAAM long range missiles. It can carry a maximum load of 24,500 pounds (11,113 kilograms) of bombs and missiles for ground attack.

McDonnell Douglas F-15E-47-MC Eagle 89-0487, at Lakenheath, 19 October 2019. The aircraft was photographed by Bradley Bygrave, and the image is used with permission.

© 2020, Bryan R. Swopes