Tag Archives: World Record for Speed Over a 15km/25km Straight Course

3 June 1953

Jackie Cochran in teh cocpit of the Canadair CL-13 Sabre Mk.3, No. 19200, on Rogers Dry Lake, May 1953. (LIFE Magazine via Jet Pilot Overseas)
Jackie Cochran in the cockpit of the Canadair CL-13 Sabre Mk.3, No. 19200, on Rogers Dry Lake, May 1953. (J. R. Eyerman/LIFE Magazine)

3 June 1953: Concluding a series of speed and altitude records, Jackie Cochran set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15-to-25 Kilometer Straight Course with an average speed of 1,067.68 kilometers per hour (663.43 miles per hour) while flying the Canadair CL-13 Sabre Mk.3 No. 19200 at Edwards Air Force Base, California.¹

In the previous weeks, Jackie Cochran had flown the experimental Orenda-powered Sabre to world records over the 100 and 500 kilometer closed circuit and set an altitude record of 14,377 meters (47,169 feet).² During these flights, she became the first woman to “break the sound barrier” when the Sabre Mk. 3 exceeded Mach 1.

On the morning of 3 June, Cochran had attempted to set a new world record over the 3 kilometer straight course, which was flown at an altitude of 200 feet (61 meters). After two runs she determined that the Sabre Mk.3 would not exceed the previous record, and she abandoned the attempt.

In her autobiography, she wrote:

The plane was immediately refueled and the timing devices were shifted to the 15-kilometer course. That took about two hours and the roughness in the air was building up by the minute. A pass in each direction over the 15-kilometer course was needed for an average speed, as against four passes over the 3-kilometer course. I had fuel enough for four passes. The average of any two consecutive passes could be taken. The first pass from south to north was at a speed of 680 miles per hour. That result was relayed to me by air from my own Lodestar, which was parked on the lake bed near the judges’ equipment. The second pass from north to south, with the wind against me, was at a speed of 670 miles per hour. I determined to make a third pass, even though the plane had developed a bad left-wing down roll at high speed and was in consequence next to unmanageable over the level flight course and its approaches. On this third pass I decided to take a long dive at the conclusion of which I would level out before reaching the approach to the course. I did this but, on leveling out, the controls again “froze” on me with the plane determined to roll over to the left. I used both arms to pull on the controls and one knee as well for leverage but with no effect. Another second or two and the plane would have been over on its back and into the ground. I prevented this only by slowing it down. At the moment I pulled back on the power there was an automatic temporary compensation of the direction of the plane to the right of the course and, as a result, the timing camera did not catch me on that third pass. That ended the flight. I made a long turn for landing and “Chuck” Yeager, in his chase plane, closed in behind me. He instructed me to leave the throttle untouched as much as possible and to land on the lake bed. I wanted to put the plane down on the runway where the ground crew was waiting but “Chuck” insisted that I put it down on the lake bed where I could take a high-speed landing and a long roll. I took my oxygen mask off and smelled fuel in the cockpit. When the wheels touched ground and the roll had about stopped, “Chuck” told me to cut the throttle and switches and get out as quickly as possible because I had a bad fuel leak which he had seen from his plane. A stream of fuel about the size of one’s thumb was gushing out of the bottom of the main section of the left wing. . . .

The Stars at Noon, by Jacqueline Cochran, Little, Brown and Company, Boston, 1954, Chapter XII, at Pages 232–233.

Major Charles E. Yeager, U.S. Air Force, and Jacqueline Cochran with the Canadair CL-13 Sabre Mk.3. Chuck Yeager and Jackie Cochran were the very best of friends. (LIFE Magazine via Jet Pilot Overseas)
Major Charles E. Yeager, U.S. Air Force, and Jacqueline Cochran with the Canadair CL-13 Sabre Mk.3. Chuck Yeager and Jackie Cochran were the very best of friends. (LIFE Magazine via Jet Pilot Overseas)

The Canadair Sabre Mk.3 was a one-of-a-kind CL-13 Sabre (an F-86E Sabre manufactured by Canadair Ltd. under license from North American Aviation, Inc.) built to test the prototype Avro Canada Gas Turbine Division Orenda 3 engine. Modifications to the F-86 airframe were required to install the new, larger engine.

The Orenda 3 was an axial-flow turbojet engine with a 10-stage compressor, six combustion chambers and single-stage turbine. It produced 6,000 pounds of thrust (16.69 kilonewtons), a 15% improvement over the General Electric J47-GE-13 installed in the standard F-86E. The Orenda was 121.3 inches (3.081 meters) long, 42 inches (1.067 meters) in diameter and weighed 2,650 pounds (1,202 kilograms).

Canadair Ltd. was an aircraft manufacturer located at Cartierville, Montreal, Canada, owned by the American submarine builder, Electric Boat Company. Canadair also built licensed versions of the Douglas DC-4 (powered by Rolls-Royce Merlin engines) and the Lockheed T-33 two-place jet trainer. In 1954, the company became a part of General Dynamics.

After the speed and altitude records, No. 19200 was sent to North American Aviation for evaluation. Today, it is on static display outdoors at Wetaskiwin Regional General Airport (CEX3), Alberta, Canada.

Jackie Cochran in the cockpit of the Canadair Sabre Mk.3 No. 19200 at Edwards AFB. (LIFE Magazine)
Jackie Cochran in the cockpit of the Canadair Sabre Mk.3 No. 19200 on the dry lake bed at Edwards Air Force Base. (LIFE Magazine via Jet Pilot Overseas)

¹ FAI Record File Number 8870

² FAI Record File Numbers 13039, 13040, 9075, 9076 and 12858

© 2019, Bryan R. Swopes

3 June 1946

National Aeronautic Association official observers check Keith Wilson’s Sikorsky R-5A as it approaches the finish line of the 20-kilometer course, establishing a new FAI speed record. (The Dayton Herald, Vol. 67, No. 130, 3 June 1946, Page 1, Columns 5–6)

3 June 1946: As part of a series of world record attempts made over a three-day period by the United States Army Air Forces, Lieutenant Colonel Keith S. Wilson, Chief of the Rotary Wing Branch of the Air Material Command at Wright Field, took off at 9:01 a.m., and flew a Sikorsky R-5A helicopter over a 20 kilometer (12.4 statute miles) course. The helicopter completed the course in 6 minutes, 43 seconds. This established a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15/25 Kilometer Straight Course of 178.39 kilometers per hour (110.85 miles per hour).¹ This exceeded the previous record which had been set by Ewald Rholfs, 25 June 1937, with a prototype Focke-Wulf 61.²

“CRANING NECKS to see the Sikorsky R-5A helicopter cross the starting line at Wright Field this morning on its way to hanging up a new speed record, these official timers and timer-observers, stand with stop watches in hand. They are (left to right): Stephen Wolfe, W. G. Kiefaber, George Baker, L. L. Custer, official timer; Russell Nichols technical director of National Aeronautic Association (NAA), Lt. Col. R. G., Ruegg, project officerf for all record flights, and Maj. P.G. Atkinson, who holds a similar title in Washington.” (The Dayton Herald, Vol. 67, No. 130, 3 June 1946, Page 1, Columns 4–6)

The National Aeronautic Association official observers of the record flight were Stephern Wolfe, L.L. Custer, and W.G. Kiefaber, timeres; Russell Nichols NAA Technical Director.

Lieutenant Colonel Wilson was awarded the Legion of Merit:

The President of the United States of America, authorized by Act of Congress, 20 July 1942, takes pleasure in presenting the Legion of merit to Lieutenant Colonel (Air Corps) Keith S. Wilson, United States Army Air Forces, for exceptionally meritorious conduct in the performance of outstanding service to the Government of the United States from January 1945 to March 1947.

Sikorsky XR-5 48-28237, the second XR-5 prototype. (NASM)

The Sikorsky R-5A (Model S-48) was a single-engine, two-place helicopter. The cabin was built of aluminum with plexiglas windows. The fuselage was built of plastic-impregnated plywood and the tail boom was wood monocoque construction. The main rotor consisted of three fully-articulated blades built of wood spars and ribs and covered with fabric. The three bladed semi-articulated tail rotor was built of laminated wood. The main rotor turned counter-clockwise as seen from above. (The advancing blade is on the helicopter’s right.) The tail rotor was mounted on the helicopter’s left side in a pusher configuration. It turned clockwise as seen from the helicopter’s left.

The R-5A went into production in July 1945 and more than 300 had been built by the time production ended in 1951.

The helicopter’s fuselage was 41 feet, 7½ inches (12.687 meters) long. The main rotor had a diameter of 48 feet, 0 inches (14.630 meters) and tail rotor diameter was 8 feet, 5 inches (2.565 meters), giving the helicopter an overall length of 57 feet, 1 inch (17.399 meters) with rotors turning. It was 13 feet, 1½ inches (4.001 meters) high. The landing gear tread was 12 feet (3.7 meters). The R-5A had an empty weight of 3,780 pounds (1,715 kilograms) and maximum takeoff weight of 4,900 pounds (2,223 kilograms). Fuel capacity was 100 gallons (378.5 liters).

Three-view illustration of Sikorsky S-48 (R-5) with dimensions. (Sikorsky Historical Archives)

The helicopter was powered by an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liter) Pratt & Whitney Wasp Jr. T1B4 (R-985 AN-5) direct-drive, nine-cylinder radial engine which was placed vertically in the fuselage behind the crew compartment. This engine was rated at 450 horsepower at 2,300 r.p.m., Standard Day at Sea Level. The R-985 AN-5 was 4 feet, 0.00 inches (1.219 meters) long, 3 feet, 10.25 inches (1.175 meters) in diameter and weighed 684 pounds (310.3 kilograms) with a magnesium crankcase.

The R-5 had a maximum speed (Vne) of 107 knots (123.1 miles per hour/198.2 kilometers per hour). Range was 275 miles (442.6 kilometers). The service ceiling was 14,800 feet (4,511 meters). The absolute hover ceiling was 3,000 feet (914.4 meters).

¹ FAI Record File Number 13157

² FAI Record File Number 13063: 122,55 km/h (76.15 m.p.h.)

Focke-Wulf Fw 61 V2 (Fédération Aéronautique Internationale)

© 2021, Bryan R. Swopes

31 May 1955

Jacqueline Auriol devant le Mystère IV, en juillet 1955. L'avion a servi de modèle au collier vendu aux enchères mardi 13 mai 2014 à Genève. [AP Photo/Str - Keystone]
Jacqueline Auriol devant le Mystère IV, en juillet 1955. L’avion a servi de modèle au collier vendu aux enchères mardi 13 mai 2014 à Genève. [AP Photo/Str – Keystone]
31 May 1955: Test Pilot Jacqueline Marie-Thérèse Suzanne Douet Auriol flew the Dassault MD.454 Mystère IV N to a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15-to-25 Kilometer Straight Course at Brétigny-sur-Orge, France.¹ Her average speed of 1,151 kilometers per hour (715 miles per hour)—0.94 Mach—broke the previous record which had been set two years earlier by her friend, Jacqueline Cochran.

Jacqueline Auriol was awarded the Harmon International Trophy for 1955, the third of four that she would receive.

Dassault Mystere IV N 01
Dassault MD.454 Mystère IV N 01. (Weygand Collection via FrenchWings.net) 

The Société des Avions Marcel Dassault MD.454 Mystère IV N 01 was the first of two prototype two-place, single-engine, swept-wing interceptors. 01 was first flown 19 July 1954 by test pilot Gérrard Muselli. It had a large air-search radar mounted over the intake and was armed with 52 rockets carried in a retractable tray in the belly, very similar to the North American Aviation F-86D Sabre. The fuselage had been lengthened over the single-seat Mystère IV to provide space for the second cockpit.

The Mystère IV N was 49 feet, 11 inches (15.215 meters) long with a wingspan of 37 feet, 6 inches (11.430 meters) and overall height of 15 feet, 1 inch (4.597 meters). Its empty weight was 15,741 pounds (7,140 kilograms) and maximum takeoff weight was 22,572 pounds (10,238 kilograms).

Dassault Mystère IV N 01 F-ZXRM, right side profile. (© Collection Pyperpote)
Dassault Mystère IV N 01 F-ZXRM, right side profile. (© Collection Pyperpote)

The Mystère IV N was powered by a Rolls-Royce Avon RA.7R axial flow, afterburning turbojet engine. It used a 12-stage compressor, 8 combustion chambers and 2-stage turbine. It produced 9,500 pounds of thrust (42.258 kilonewtons) at 7,800 r.p.m., with afterburner. The engine was 42.2 inches (1.072 meters) in diameter, 276 inches (7.010 meters) long and weighed 2,960 pounds (1,343 kilograms).

Jacqueline Auriol’s record-setting Dassault Mystère IV N 01 F-ZXRM is on display at the Conservatoire l’Air et l’Espace d’Acquitane, Bordeaux Merignac Airport, France.

Mystère IV N aux cent ans de l'aviation de Mérignac (PA/Wikipedia)
Dassault Mystère IV N 01 on display at the Conservatoire l’Air et l’Espace d’Acquitane, Bordeaux Merignac Airport, France. (PA/Wikipedia)

¹ FAI Record File Number 9074

© 2019, Bryan R. Swopes

16 May 1958

CAPT Walter W. Irwin lands at Edwards Air Force Base, California, 16 May 1958. The airplane is Lockheed F-104A-1-LO 55-2969. (U.S. Air Force)

16 May 1958: At Edwards Air Force Base, in the high desert of southern California, Captain Walter Wayne Irwin, United States Air Force, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15-to-25 Kilometer Straight Course when he flew a Lockheed F-104A Starfighter, serial number 55-2969, to 2,259.538 kilometers per hour (1,404.012 miles per hour). ¹ He made two runs over the course at an altitude of 40,000 feet (12,192 meters). ²

On the same day, Captain Irwin set two U.S. National Aeronautic Association time-to-altitude records by flying -969 to 3,000 meters in 41.8 seconds, and to 25,000 meters in 4 minutes, 26.03 seconds. It reached a peak altitude of 27,813 meters (91,246 feet).

Captain Walter W. Irwin, United States Air Force, stands next to a Lockheed F-104. (U.S. Air Force)

Captain Irwin was part of a group of engineers and pilots awarded the Robert J. Collier Trophy by the National Aeronautic Association in 1958 for “the greatest achievement in aeronautics” because of their involvement in the Lockheed F-104 program. In a ceremony held 16 December 1958, General Benjamin Wilkey Chidlaw, former commanding general, Air Defense Command, presented the Thompson Trophy to Captain Irwin.

Vice President Richard M. Nixon presents the Collier Trophy. Left to right, Major Walter W. Irwin and Lieutenant Colonel Howard C. Johnson; Nixon; Neil Burgess and Gerhard Neumann, designers of the General Electric J79 engine; and Clarence Leonard (“Kelly”) Johnson, Lockheed Aircraft Corporation. 15 December 1959. (NASM-00142388)
Captain Walter W. Irwin, U.S. Air Force, at Edwards AFB, 16 May 1958. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

Walter Wayne Irwin was born 21 August 1924 at Everett, Washington. He was the son of John Harve Irwin, a shoe store clerk, and Stella Mildred Faulstich. He attended Wenatchee High School in Wanatchee, Washington, graduating in 1941.

Irwin enlisted as a private in the Air Corps, United States Army, at Seattle, Washington, 6 January 1942. Trained as a fighter pilot, he was commissioned as a second lieutenant 3 November 1942.

Lieutenant Irwin flew 88 combat missions in the Republic P-47 Thunderbolt with the Ninth Air Force in Europe during World War II. He was shot down, captured and held as a prisoner of war for a week before he escaped and made his way to friendly forces.

Captain Irwin married Lieutenant Christine Ann Stevens, Nurse Corps, United States Air Force, in a Catholic ceremony at Arlington, Virginia, 4 December 1954. Lieutenant Stevens was assigned to the base hospital at Travis Air Force Base in California. They would have four children.

At the time he set the record, Captain Irwin had just returned from an overseas assignment in Taiwan. He was a flight commander with the 83rd Fighter Interceptor Squadron, based at Hamilton Air Force Base, Novato, California.

In addition to the Collier Trophy, Major Irwin won the Thompson Trophy for his F-104 speed record.

Lockheed F-104A Starfighter 55-2969. The prototype Lockheed Model 188 Electra is in the photograph behind the interceptor.

Walter Irwin retired from the Air Force with the rank of colonel following thirty years of service. In retirement, he was owner of a realty company in Sebastopol, California.

On 17 April 1978, Colonel Irwin was flying a rented Piper PA-28-161 Cherokee Warrior near Occidental, California. Witnesses saw the airplane maneuvering at low altitude. A wing clipped an oak tree. The airplane crashed and caught fire. Walter Wayne Irwin was killed. His ashes were spread at sea.

Formation of two Lockheed F-104A-15-LO (S/N 56-0769 and 56-0781). (U.S. Air Force photo)

The Lockheed F-104A Starfighter was a single-place, single engine supersonic interceptor. It was designed by a team lead by the legendary Clarence L. “Kelly” Johnson.

The F-104A is 54.77 feet (16.694 meters) long with a wingspan of 21.94 feet (6.687 meters) and overall height of 13.49 feet (4.112 meters). The total wing area is just 196.1 square feet (18.2 square meters). At 25% chord, the wings are swept aft 18° 6′. They have 0° angle of incidence and no twist. The airplane has a very pronounced -10° anhedral. An all-flying stabilator is placed at the top of the airplane’s vertical fin, creating a “T-tail” configuration.

Lockheed F-104A-1-LO Starfighter 55-2969 (U.S. Air Force)
Lockheed F-104A-1-LO Starfighter 55-2969 (U.S. Air Force)

The F-104A had an empty weight of 13,184 pounds (5,980.2 kilograms). The airplane’s gross weight varied from 19,600 pounds to 25,300 pounds, depending on the load of missiles and/or external fuel tanks.

Internal fuel capacity was 896 gallons (3,392 liters). With Sidewinder missiles, the F-104A could carry two external fuel tanks on underwing pylons, for an additional 400 gallons (1,514 liters). If no missiles were carried, two more tanks could be attached to the wing tips, adding another 330 gallons (1,249 liters) of fuel.

Lockheed F-104A Starfighter three-view illustration with dimensions.

The F-104A was powered by a single General Electric J79-GE-3A engine, a single-spool axial-flow afterburning turbojet, which used a 17-stage compressor and 3-stage turbine. The J79-GE-3A is rated at 9,600 pounds of thrust (42.70 kilonewtons), and 15,000 pounds (66.72 kilonewtons) with afterburner. The engine is 17 feet, 3.5 inches (5.271 meters) long, 3 feet, 2.3 inches (0.973 meters) in diameter, and weighs 3,325 pounds (1,508 kilograms).

55-2969 in General Electric colors (Pinterest)
55-2969 in General Electric colors. (Pinterest)

The F-104A had a maximum speed of 1,037 miles per hour (1,669 kilometers per hour) at 50,000 feet (15,240 meters). Its stall speed was 198 miles per hour (319 kilometers per hour). The Starfighter’s initial rate of climb was 60,395 feet per minute (306.8 meters per second). The combat ceiling was 55,200 feet (16,825 meters) and the service ceiling was 64,795 feet (19,750 meters).

Armament was one General Electric M61 Vulcan six-barreled revolving cannon with 725 rounds of 20 mm ammunition. An AIM-9B Sidewinder heat-seeking air-to-air missile could be carried on each wing tip, or a jettisonable fuel tank with a capacity of 141.5 gallons (535.6 liters).

Lockheed built 153 of the F-104A Starfighter initial production version. A total of 2,578 F-104s of all variants were produced by Lockheed and its licensees, Canadair, Fiat, Fokker, MBB, Messerschmitt,  Mitsubishi and SABCA. By 1969, the F-104A had been retired from service. The last Starfighter, an Aeritalia-built F-104S ASA/M of the  Aeronautica Militare Italiana, was retired in October 2004.

55-2969 was one of the original pre-production Lockheed YF-104As, completed 20 August 1956. It was modified to the F-104A standard configuration and assigned to the 83rd Fighter Interceptor Squadron at Hamilton Air Force Base, near Novato, California.

On 22 August 1957 the Starfighter was damaged at Eglin Air Force Base, Florida. It was returned to Lockheed for repair and upgraded to F-104A-1. In May 1958, -969 and another Starfighter were sent to Edwards to attempt setting several speed and altitude records. They were both then returned to the 83rd FIS.

Lockheed F-104A-1-L) Starfighter 55-2969 with a General Electric J79 turbojet engine, circa 1960. General Electric)
Lockheed F-104A-1-LO Starfighter 55-2969 with a General Electric J79 turbojet engine, circa 1960. (General Electric)

From August 1958 to August 1961, -969 was loaned to General Electric to test improvements to the J79 turbojet engine. While there, it was given the name Queenie, which was painted on the nose along with three playing cards.

In 1964 55-2969 was again returned to Lockheed for conversion to a QF-104A remote-controlled target drone. It was damaged by a AIM-9 Sidewinder missile on 28 September 1968, but was recovered, repaired and returned to service. On its 25th drone mission, 26 January 1971, Queenie was shot down by an experimental XAIM-4H Falcon air-to-air missile fired by an F-4E Phantom II.

Lockheed QF-104A 55-2969
Lockheed QF-104A 55-2969 at Eglin Air Force Base circa 1969

¹ FAI Record File Number 9063

² The Speed of Sound at 40,000 feet is 659.8 miles per hour (1,062 kilometers per hour). Captain Irvin’s record average speed was Mach 2.13.

© 2020, Bryan R. Swopes

11 May 1964

Jackie Cochran and Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)
Jackie Cochran and Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)

11 May 1964: At Edwards Air Force Base, California, Jacqueline Cochran flew a Lockheed F-104G Starfighter, 62-12222, to 2,300.23 kilometers per hour (1,429.30 miles per hour)—Mach 2.16—over a straight 15 to 25 kilometer course. She was the first woman to fly faster than Mach 2 and she set a new Fédération Aéronautique Internationale (FAI) World Speed Record. ¹

Jackie Cochran taxiing Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)
Jackie Cochran taxiing Lockheed F-104G Starfighter 62-12222 at Edwards AFB, 1964. (FAI)

Jackie Cochran wrote about flying the 15/25 kilometer straight course in her autobiography:

Picture in your mind a rectangular tunnel, 300 feet high, a quarter of a mile wide, and extending 20 miles long through the air at an altitude of 35,000 feet. I had to fly through that tunnel at top speed without touching a side. There were no walls to see but radar and ground instruments let me know my mistakes immediately. Up there at 35,000 feet the temperature would be about 45 degrees below zero. Not pleasant but perfect for what I was doing. Inside the plane you are hot because of the friction of speeding through the air like that. The cockpit was air-conditioned, but when you descend, things happen so fast the plane’s air-cooling system can’t keep up with it. I was always hot and perspiring back on the ground.

Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York 1987, Page 314.

Cochran set three speed records with this F-104G in May and June 1964. Under the Military Assistance Program, the U.S. Air Force transferred it to the Republic of China Air Force, where it was assigned number 4322. It crashed 17 July 1981.

The record-setting Lockheed F-104G Starfighter, USAF serial number 62-12222, in service with the Republic of China Air Force as 4322.
The record-setting Lockheed F-104G Starfighter, USAF serial number 62-12222, in service with the Republic of China Air Force as 4322.

The F-104G was the final production version of the Lockheed Starfighter. Rather than an interceptor, the G-model was a fighter bomber, with a strengthened fuselage and wings, and hardpoints for carrying bombs and additional fuel tanks. Built by Lockheed, they were also licensed for production by Canadair, Dornier, Fiat, Fokker, Messerschmitt and SABCA.

The F-104G was a single-seat, single engine fighter bomber, 54 feet 8 inches (16.662 meters) long with a wingspan of just 21 feet, 9 inches (6.629 meters) and overall height of 13 feet, 6 inches (4.115 meters). The empty weight is 14,000 pounds (6,350.3 kilograms) and loaded weight is 20,640 pounds (9,362.2 kilograms).

The F-104G was powered by a General Electric J79-GE-11A engine, a single-spool, axial-flow, afterburning turbojet, which used a 17-stage compressor section and 3-stage turbine. The J79-GE-11A is rated at 10,000 pounds of thrust (44.48 kilonewtons), and 15,800 pounds (70.28 kilonewtons) with afterburner. The engine is 17 feet, 4.0 inches (5.283 meters) long, 3 feet, 2.3 inches (0.973 meters) in diameter, and weighed 3,560 pounds (1,615 kilograms).

The maximum speed is 1,328 miles per hour (2,137.2 kilometers per hour). It has a combat radius of 420 miles (675.9 kilometers) or a ferry range of 1,630 miles (2,623.2 kilometers) The service ceiling is 50,000 feet (15,240 meters).

General Electric M61A1 20 mm rotary cannon in the weapons bay of a Lockheed F-104G Starfighter. (Michael Wolf/Wikipedia)
General Electric M61A1 20 mm rotary cannon in the weapons bay of a Lockheed F-104G Starfighter. (Michael Wolf/Wikipedia)

Armament consists of a 20 mm General Electric M61A1 Vulcan six-barreled Gatling gun, with 725 rounds of ammunition. Up to four AIM-9 Sidewinder air-to-air heat seeking missiles can be carried on the wingtips or under wing pylons. In place of missiles, two wingtip fuel tanks and another two under wing tanks could be carried.

On NATO alert, the F-104G was armed with a B43 variable-yield nuclear bomb mounted on the fuselage centerline hardpoint. The B43 could be set for explosive force between 170 kilotons and 1 megaton.

Two F-104G Starfighters in service with the Luftwaffe. The airplane closest to the camera, marked 26+41, was built by Messerschmitt with final assembly by MBB-Manching in February 1971. (© Peter Doll)
Two F-104G Starfighters in service with the Luftwaffe. The airplane closest to the camera, marked 26+41, was built by Messerschmitt with final assembly by MBB-Manching in February 1971. (© Peter Doll)

¹ FAI Record File Number 13041

© 2017, Bryan R. Swopes