Tag Archives: General Electric Trophy

4 September 1955

Three Boeing B-47E Stratojet strategic bombers assigned to the 306th Bombardment Wing (Medium), based at MacDill AFB, Florida. The airplane closest to the camera is Boeing-Wichita-built B-47E-95-BW 52-0545. The lead aircraft is Lockheed-Marietta-built B-47E-25-LM 52-0250. These aircraft are similar in appearance to the B-47s flown in the 1955 General Electric Trophy Race. (U.S. Air Force)

4 September 1955: Three Boeing B-47 Stratojet strategic bombers raced from March Air Force Base near Riverside, California, to Philadelphia International Airport, Philadelphia, Pennsylvania, in competition for the General Electric Trophy. They departed from March Field at ten minute intervals beginning at 3:30 a.m. Pacific Standard Time (11:30 UTC).  The winning bomber was the third to takeoff.

The winning airplane, B-47B-50-BW 51-2314, assigned to the 443d Bombardment Squadron (Medium), 320th Bombardment Wing (Medium), 15th Air Force, completed the 2,337 miles (3,761 kilometers) course in 3 hours, 57 minutes, 59.2 seconds, averaging 589.294 miles per hour (948.377 kilometers per hour).

A Boeing B-47B-50-BW Stratojet, 51-2307, assigned to the 320th Bombardment Wing (Medium) (denoted by the two diagonal stripes on its tail) at March Air Force Base, California, circa 1953. This is the same type aircraft that won the 1955 General Electric Trophy. (U. S Air Force)

The second-place B-47, (probably an RB-47E) from the 3rd Strategic Reconnaissance Squadron, 26th Strategic Reconnaissance Wing, Lockbourne AFB, located east of Columbus, Ohio, finished with an average speed of 585.263 miles per hour (941.890 kilometers per hour). The third-place Stratojet, assigned to the 306th Bombardment Wing (Medium), MacDill AFB, near Tampa, Florida, finished with a speed of 584.167 miles per hour (940.127 kilometers per hour). (B-47s of the 306th were featured prominently in the 1955 motion picture, “Strategic Air Command.”)

Great Circle Course from March AFB, California, to Philadelphia International Airport, Pennsylvania, 2,342 statute miles (3,769 kilometers). (Great Circle Mapper)

A crowd of spectators, estimated to number about 60,000, was present to see the finish of the race.

The race was timed by officials of the National Aeronautic Association. The chief timer was Roger Wolfe Kahn.¹

—AP Wirephoto, Democrat and Chronicle, Rochester, New York, 5 September 1955, Page 1, Columns 3–5

The winning four-man crew consisted of Major Leonard J. Stevens, aircraft commander; Major Freeman J. Weedman, co-pilot; Captain Glenn J. Fornes, navigator; and Staff Sergeant James P. Flohe, crew chief. The second-place B-47 was flown by Maj. William E. Yingling, aircraft commander; Lieutenant Herbert M. Plynter, co-pilot; Captain Joseph D. Brown, navigator; and Airman 1st Class P. J. Clemons, crew chief. The third-place bomber was flown by Lieutenant Colonel Warren H. Smith, Jr., aircraft commander; Captain John S. Schrader, co-pilot, Major John E. Terry, navigator; and Master Sergent Carlton Spiers, crew chief.

On the same day, four North American Aviation F-100C Super Sabres competed in the Bendix Trophy Race from George AFB, California, to Philadelphia. The average speed of the fourth-place Super Sabre was slower than that of all three B-47s, and 23.843 miles per hour (38.372 kilometers per hour) slower than the GE Trophy winning B-47. (It should be noted, though, that the F-100s had to make two fuel stops during their cross-country flight, while the B-47s flew the course non-stop.)

A Boeing B-47B Stratojet rocket-assisted takeoff (ATO). The black smoke from the engines indicates water-methanol injection is in use. 15 April 1954. (U.S. Air Force 061024-F-1234S-011)

Designed by Boeing, the Stratojet was a high-subsonic-speed strategic bomber and reconnaissance aircraft, in service from 1951 until 1977. The B-47 could fly higher and faster than jet fighters of the time, and it was also highly maneuverable. The B-47 was flown by a two pilots in a tandem cockpit. A navigator/bombardier was at a station in the nose.

The Boeing B-47B Stratojet was the first full-production model. The B-47B is 106 feet, 10 inches (32.563 meters) long with a wingspan of 116 feet, 0 inches(35.357 meters), and an overall height of 27 feet, 11 inches (8.509 meters). The wings are shoulder-mounted with the leading edges swept aft to 36° 37′. Their angle of incidence is 2° 45′ and there is no dihedral. (The wings are very flexible, showing marked anhedral on the ground and flexing upward when in flight.) The B-47B has an empty weight of 78,102 pounds (35,426 kilograms), and a maximum takeoff weight of 185,000 pounds (83,915 kilograms). The maximum in-flight weight (after air refueling) was 221,000 pounds (100,244 kilograms).

From 1953 to 1957, the B-47B fleet underwent an extensive modification program which brought them up to the B-47E configuration.

The B-47B was originally powered by six General Electric J47-GE-11 turbojet engines in four nacelles mounted on pylons below the wings. All B-47Bs after serial number 51-2046 were equipped with J47-GE-23 engines. The airplanes built with the -11 engines were retroffitted with the -23s. Under the modification and upgrade program, the -23s were replaced by the J47-GE-25. This engine has a 12-stage axial-flow compressor, eight combustion chambers, and single-stage turbine. The J47-GE-25 is rated at 5,970 pounds of static thrust at Sea Level, at 7,950 r.p.m. and 1,250 °F. (677 °C.) turbine outlet temperature (TOT). (7,200 pounds of thrust with water injection). It has a maximum diameter of 3 feet, 1 inch (0.940 meters), length of 12 feet, 0 inches (3.658 meters) and weighs 2,653 pounds (1,203 kilograms).

The B-47B was also equipped with solid-fuel rocket engines (JATO) located in the aft fuselage. These produced a maximum 33,000 pounds of thrust (146.8 kilonewtons) for 14 seconds.

The B-47B Stratojet had a cruise speed of 433 knots (498 miles per hour/802 kilometers per hour), and maximum speed of 528 knots (608 miles per hour/978 kilometers per hour) at 16,300 feet (4,968 meters). The service ceiling was 42,100 feet (10,333 meters) and combat ceiling 40,800 feet (12,436 meters).

The combat radius of the B-47B was 1,704 nautical miles (1,961 statute miles/3,156 kilometers) with a 10,000 pound (4,536 kilograms) bomb load. Two jettisonable underwing fuel tanks could carry 1,780 gallons (6,738 liters) each. The maximum ferry range was 3,861 nautical miles (4,443 statute miles (7,151 kilometers).

Boeing B-47E-55-BW Stratojet 51-2394, similar in appearance to bombers in the 1955 General Electric Trophy Race. Photographed 7 April 1956. (U.S. Air Force)

For defense the B-47B was armed with two Browning AN-M3 .50-caliber machine guns in a remotely-operated tail turret, with 600 rounds of ammunition per gun. The co-pilot acted as the gunner using an optical sight. The machine guns were later replaced by two M24A1 20 mm autocannons and radar control.

The maximum bomb load of the B-47B was 18,000 pounds (8,165 kilograms). The B-47 could carry two 7,600 pound (3,447 kilogram) Mark 15 two-stage radiation implosion thermonuclear bombs, each with an explosive yield of up 3.8 megatons, depending on the version, or a single 10,670 pound (4,808 kilogram) B-41 three-stage, 25 megaton bomb.

Beginning in 1953, the B-47B fleet underwent an extensive modification program which brought them up to the B-47E configuration.

A total of 2,032 B-47s were built by a consortium of three aircraft manufacturers: Boeing Airplane Company, Wichita, Kansas; Douglas Aircraft Company, Tulsa, Oklahoma; Lockheed Aircraft Company, Marietta, Georgia. 399 of these were B-47Bs.

The Stratojet is one of the most influential aircraft designs of all time and its legacy can be seen in almost every jet airliner built since the 1950s: the swept wing with engines suspended below and ahead on pylons. The B-47 served the United States Air Force from 1951 to 1977. From the first flight of the Boeing XB-47 Stratojet prototype, 17 December 1947, to the final flight of B-47E 52-166, was 38 years, 6 months, 1 day.

The General Electric Trophy winner, B-47B 51-2314, was sent to The Boneyard at Davis-Monthan Air Force Base, Tucson, Arizona, 16 December 1960.

This Day in Aviation would like to express great thanks to Mr. A. W. Greenfield, Director, Contest & Records Board, National Aeronautic Association, for his help in researching this article.

Boeing RB-47E-1-BW Stratojet, 51-5259—the reconnaissance variant. (U.S. Air Force)

¹ Roger Wolff Kahn (19 October 1907–12 July 1962) was a jazz musician, composer and band leader. He was featured on the cover of TIME Magazine, 19 September 1927. Kahn also had a life-long interest in aviation. In 1933, he became a test pilot for the Grumman Aircraft Engineering Corporation. Following World War II, as director of Grumman’s Department of Service and Product Support, he flew a custom-built Grumman G-58B, a civilian version of the Grumman F8F-2 Bearcat. He was the vice president of the Institute of Aeronautical Sciences, and served as chairman of the National Aeronautic Association. He had logged more than 7,000 flight hours.

Roger Wolfe Kahn (IMDb)
© 2023, Bryan R. Swopes

2 September 1956

Three Boeing B-47E Stratojet strategic bombers assigned to the 306th Bombardment Wing. The airplane closest to the camera is Boeing-Wichita-built B-47E-95-BW 52-0545. The lead aircraft is Lockheed-Marietta-built B-47E-25-LM 52-0250. These aircraft are similar to the B-47s flown in the 1955 General Electric Trophy Race. (U.S. Air Force)

2 September 1956: As it had been the previous year, the 1956 General Electric Trophy Race was flown by three Boeing B-47 Stratojet strategic bombers. The 1955 race course was from March Air Force Base, California, to Philadelphia International Airport in Pennsylvania. The 1956 course was changed so that the competitors would be facing headwinds rather than tailwinds. The race began at Kindley Air Force Base, St. David’s Island, Bermuda, and ended at Will Rogers Field, Oklahoma City, Oklahoma.

An estimated 100,000 spectators were present to see the finish of the race. The winning B-47, flown by Major Joseph Schreiber, 33d Bombardment Squadron (Medium), 22d Bombardment Wing (Medium), based at March Field, arrived overhead at 11:38 a.m. Its official time for the course was 3 hours, 8 minutes, 43.6 seconds, with an average speed of 601.187 miles per hour (967.517 kilometers per hour).

Major Schreiber had flown a Great Circle Course. He flew at 12,000 to 20,000 feet (3,658–6,096 meters), searching for the most favorable winds. During the flight, the B-47 encountered headwinds of up to 45 miles per hour (20 meters per second).

Great Circle Course from Kindley Air Force Base, Bermuda, to Will Rogers Field, Oklahoma, 1,895 statute miles (3,050 kilometers). (Great Circle Mapper)

The crew of Schreiber’s B-47 included Captain Denis O. Wilson, co-pilot; Major Christian J. Luecke, navigator; and Technical Sergeant James Richardson, crew chief.

The second place aircraft, a B-47E assigned to the 301st Bombardment Wing (Medium), 22d Bombardment Wing (Medium), 2nd Air Force, at Barksdale AFB, trailed Major Schreiber’s aircraft by 21 seconds. It was flown by Lieutenant Colonel John C. Lewis; Captain John D. Roche; Lieutenant Colonel Oscar R. Black; and Staff Sergeant Thomas J. Tharo. Colonel Lewis had to slow down when a row of rivets on a left wing engine nacelle popped and a piece of skin was torn off. Its time at the finish line was 3 hours, 9 minutes, 49 seconds, for an average speed of 600.058 miles per hour (965.700 kilometers per hour).

The third-place B-47, assigned to the 310th Bombardment Wing (Medium) at Smoky Hill AFB, Salina, Kansas, was flown by Captain C. L. Porter, Captain R. W. Cain, Captain Sam Allison; and crew chief Frank B. Johnston. Its finishing time was 3 hours, 11 minutes, 38 seconds, with an average speed of 593.602 miles per hour (955.310 kilometers per hour).

All three B-47s encountered significant turbulence when descending toward Will Rogers Field.

Boeing B-47E Stratojet 51-2394, similar to bombers in the 1956 General Electric trophy Race. Photographed 7 April 1956. This airplane was assigned to the 22d Bombardment Wing Medium). (U.S. Air Force)

© 2023, Bryan R. Swopes

1 September 1953

Captain Harold E. "Tom" Collins, U.S. Air Force, in the cockpit of the FAI World Speed Record setting North American Aviation F-86D-35-NA Sabre 51-6145. (Photograph courtesy of Neil Corbett, Test and Research Pilots and Flight Test Engineers)
Captain Harold E. “Tom” Collins, U.S. Air Force, in the cockpit of the FAI World Speed Record setting North American Aviation F-86D-35-NA Sabre 51-6145. (Photograph courtesy of Neil Corbett, Test and Research Pilots and Flight Test Engineers)

1 September 1953: Captain Harold Edward Collins, United States Air Force, flying North American Aviation F-86D-35-NA Sabre, 51-6145, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15-to-25 Kilometer Straight Course of 1,139.219 kilometers per hour (707.878 miles per hour) at Vandalia, Ohio.¹

North American Aviation F-86D-35-NA Sabre 51-6145, FAI World Speed Record holder.
North American Aviation F-86D-35-NA Sabre 51-6145, FAI World Speed Record holder.

This same F-86D (North American Aviation serial number 173-289) flown by Lieutenant Colonel William F. Barnes, set an FAI World Record for Speed Over a 3 Kilometer Straight Course of 715.697 miles per hour (1,151.803 kilometers per hour), 16 July 1953 at the Salton Sea, California. (FAI Record File Number 9868)

The F-86D was an all-weather interceptor developed from North American Aviation F-86 Sabre day fighter. It was the first single-seat interceptor, and it used a very sophisticated—for its time—electronic fire control system. It was equipped with search radar and armed with twenty-four unguided 2.75-inch (69.85 millimeter) Mk 4 Folding-Fin Aerial Rockets (FFAR) rockets carried in a retractable tray in its belly.

The aircraft was so complex that the pilot training course was the longest of any aircraft in the U.S. Air Force inventory, including the Boeing B-47 Stratojet.

North American Aviation F-86D-1-NA Sabre
North American Aviation F-86D-1-NA Sabre 50-463, the eighth production aircraft. (North American Aviation, Inc.)

The F-86D was larger than the F-86A, E and F fighters, with a longer and  wider fuselage. It was also considerably heavier. The day fighter’s sliding canopy was replaced with a hinged “clamshell” canopy. A large, streamlined radome was above the reshaped engine intake.

The F-86D Sabre was 40 feet, 3¼ inches (12.275 meters) long with a wingspan of 37 feet, 1½ inches (11.316 meters), and overal height of 15 feet, 0 inches (4.572 meters). The interceptor had an empty weight of 13,518 pounds (6,131.7 kilograms), and maximum takeoff weight of 19,975 pounds (9,060.5 kilograms). It retained the leading edge slats of the F-86A, F-86E and early F-86F fighters. The horizontal stabilizer and elevators were replaced by a single, all-moving stabilator. All flight controls were hydraulically boosted. A “clamshell” canopy replaced the sliding unit of earlier models.

The F-86D was powered by a General Electric J47-GE-17 engine. This was a single-shaft, axial-flow turbojet with afterburner. The engine had a 12-stage compressor, 8 combustion chambers, and single-stage turbine. The J47-GE-17 was equipped with an electronic fuel control system which substantially reduced the pilot’s workload. It had a normal (continuous) power rating of 4,990 pounds of thrust (22.20 kilonewtons); military power, 5,425 pounds (24.13 kilonewtons) (30 minute limit), and maximum 7,500 pounds of thrust (33.36 kilonewtons) with afterburner (15 minute limit). (All power ratings at 7,950 r.p.m.) It was 18 feet, 10.0 inches (5.740 meters) long, 3 feet, 3.75 inches (1.010 meters) in diameter, and weighed 3,000 pounds (1,361 kilograms).

The maximum speed of the F-86D was 601 knots (692 miles per hour/1,113 kilometers per hour) at Sea Level, 532 knots (612 miles per hour/985 kilometers per hour) at 40,000 feet (12,192 meters), and 504 knots (580 miles per hour/933 kilometers per hour)at 47,800 feet (14,569 meters).

A potential adversary of the North American Aviation F-86D Sabre all-weather interceptor was the Tupolev Tu-85 long-range strategic bomber.

The F-86D had an area intercept range of 241 nautical miles (277 statute miles/446 kilometers) and a service ceiling of 49,750 feet (15,164 meters). The maximum ferry range with external tanks was 668 nautical miles (769 statute miles/1,237 kilometers). Its initial rate of climb was 12,150 feet per minute (61.7 meters per second) from Sea Level at 16,068 pounds (7,288 kilograms). From a standing start, the F-86D could reach its service ceiling in 22.2 minutes.

The F-86D was armed with twenty-four 2.75-inch (69.85 millimeter) unguided Folding-Fin Aerial Rockets (FFAR) with explosive warheads. They were carried in a retractable tray, and could be fired in salvos of 6, 12, or 24 rockets. The FFAR was a solid-fuel rocket. The 7.55 pound (3.43 kilogram) warhead was proximity-fused, or could be set for contact detonation, or to explode when the rocket engine burned out.

The F-86D’s radar could detect a target at 30 miles (48 kilometers). The fire control system calculated a lead-collision-curve and provided guidance to the pilot through his radar scope. Once the interceptor was within 20 seconds of its target, the pilot selected the number of rockets to fire and pulled the trigger, which armed the system. At a range of 500 yards (457 meters), the fire control system launched the rockets.

North American Aviation F-86D-60-NA Sabre 53-4061 firing a salvo of  FFARs.

Between December 1949 and September 1954, 2,505 F-86D Sabres (sometimes called the “Sabre Dog”) were built by North American Aviation. There were many variants (“block numbers”) and by 1955, almost all the D-models had been returned to maintenance depots or the manufacturer for standardization. 981 of these aircraft were modified to a new F-86L standard. The last F-86D was removed from U.S. Air Force service in 1961.

After its service with the United States Air Force, the record-setting Sabre 51-6145 was transferred to a NATO ally, the Ellinikí Vasilikí Aeroporía (Royal Hellenic Air Force).

North American Aviation F-86D-20-NA Sabre (U.S. Air Force)
North American Aviation F-86D-20-NA Sabre 51-3045. (U.S. Air Force)

¹ FAI Record File Number 8869

© 2018, Bryan R. Swopes