Tag Archives: Mackay Trophy

26 May 1961

Aviation, , , , , , , , , , , , , , , , , ,
The flight crew of the Convair B-58A-10-CF Hustler 59-2451, "The Firefly," planning the Washington, D.C.-to-Paris flight, 26 May 1961. Left to right, Captain William L. Polhemus, Captain Raymond R. Wagener and Major William R. Payne. (Jet Pilot Overseas)
The flight crew of the Convair B-58A-10-CF Hustler 59-2451, “The Firefly,” planning the Washington, D.C.-to-Paris flight, 26 May 1961. Left to right, Captain William L. Polhemus, Captain Raymond R. Wagener and Major William R. Payne. (Jet Pilot Overseas)

26 May 1961: The Firefly, the Blériot Trophy-winning Convair B-58A-10-CF Hustler, serial number 59-2451, assigned to the 43rd Bombardment Wing, Carswell Air Force Base, Fort Worth, Texas, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Recognized Course by flying from Washington, D.C. to Paris in 3 hours, 39 minutes, 49 seconds, for an average speed of 1,687.69 kilometers per hour (1,048.68 miles per hour).¹

During the same flight, the B-58 flew the New York to Paris segment in 3 hours, 14 minutes, 44.53 seconds, at an average speed of 1,753.16 kilometers per hour (1,089.36 miles per hour).

The aircrew, Major William R. Payne, Aircraft Commander, Captain William L. Polhemus, Navigator, and Captain Raymond R. Wagener, Defensive Systems Officer, won the Harmon and Mackay Trophies for this flight.

Convair B-58A-10-CF Hustler 59-2451, The Firefly, lands at le Bourget, Paris, after the record-setting transatlantic flight, 26 May 1961. (University of North Texas Libraries)
Convair B-58A-10-CF Hustler 59-2451, The Firefly, lands at Aéroport de Paris – Le Bourget, Paris, after the record-setting transatlantic flight, 26 May 1961. (University of North Texas Libraries)
The Blériot Trophy, photographed 12 June 1961. “Side view of The Blériot Trophy on display. It is the figure of a naked man made of black marble in a flying position emerging from clouds. The clouds are white stone and are the figures of women in various poses on top of a marble dome.” (University of North Texas Libraries)
The Mackay Trophy.
The Mackay Trophy
The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)
The Harmon International Trophy at the Smithsonian Institution National Air and Space Museum. (NASM)

On 3 June 1961, while enroute home, The Firefly crashed only 5 miles from Paris, killing the Blériot Trophy-winning  aircrew, Major Elmer E. Murphy, Major Eugene Moses, and First Lieutenant David F. Dickerson. The B-58 was totally destroyed.

Convair B-58A-10-CF Hustler 59-2451, The Firefly.
Convair B-58A-10-CF Hustler 59-2451, The Firefly.

The B-58A Hustler was a high-altitude Mach 2 strategic bomber which served with the United States Air Force from 1960 to 1970. It was crewed by a pilot, navigator/bombardier and a defensive systems operator, each located in individual cockpits. The aircraft had a delta-winged configuration similar to the Convair F-102A Delta Dagger and F-106 Delta Dart supersonic interceptors. The fuselage incorporates the “Area Rule” which resulted in a “wasp waist” or “Coke bottle” shape for a significant reduction in aerodynamic drag. The airplane’s only control surfaces are two “elevons” and a rudder. There are no flaps.

The “Hustler” was 96.8 feet (29.5 meters) long, with a wing span of 56.8 feet (17.3 meters) and an overall height of 31.4 feet (9.6 meters). The wings’ leading edges were swept back at a 60° angle. The wings had a 3°0′ angle of incidence, 2°14′ dihedral, and a total area of 1,542.5 square feet (143.3 square meters).

The B-58A had an empty weight of 51,061 pounds (23,161 kilograms). Its Maximum Takeoff Weight (MTOW) was 90,000 pounds (40,823 kilograms), but once airborne, it could take on additional fuel from a tanker, raising the bomber’s maximum weight to 125,147 pounds (56,766 kilograms).

The B-58A was powered by four General Electric J79-GE-5 afterburning turbojet engines, suspended under the wings from pylons. These were single-shaft axial-flow engines with a 17-stage compressor and 3-stage turbine. The J79-GE-5 had a continuous power rating of 9,700 pounds of thrust (43.15 kilonewtons), Military Power, 10,000 pounds of thrust (44.49 kilonewtons), and Maximum Power, 15,600 pounds (69.39 kilonewtons) with afterburner. (All ratings at 7,460 r.p.m.) The engine was 16 feet, 10.2 inches (5.131 meters) long and 3 feet, 2.0 inches (0.889 meters) in diameter. It weighed 3,570 pounds (1,619 kilograms).

The bomber had a cruise speed of 626 miles per hour (1,007 kilometers per hour) from 30,000 to 50,000 feet (9,144–15,240 meters), and a maximum speed of 1,319 miles per hour (2,124 kilometers per hour) at 56,100 feet (17,099 meters). The B-58’s service ceiling was 67,200 feet (20,483 meters).

Jet fuel (JP-4) was carried in three tanks inside the airplane’s fuselage, and two tanks in a streamlined drop tank. The total capacity of the five tanks was 15,369 gallons (58,178 liters). Its combat radius was 2,589 miles (4,167 kilometers) and the maximum ferry range was 6,483 miles (10,434 kilometers).

The B-58 weapons load was a combination of W-39, B43 or B61 nuclear bombs. The W-39 was carried in the centerline pod. (A two-component mission pod was also available.) The W-39 was the same warhead used on the PGM-11 Redstone intermediate range ballistic missile and the SM-62 Snark intercontinental cruise missile. It was a two-stage radiation-implosion thermonuclear warhead with an explosive yield of 3.8 megatons. The warhead weighed 6,230 pounds (2,826 kilograms). The B-43 and B-61 bombs were carried on four hardpoints under the fuselage.

There was a defensive General Electric M61 Vulcan 20 mm rotary cannon mounted in the bomber’s tail, with a maximum 1,040 rounds of ammunition. The gun was remotely-controlled by the Defensive Systems Officer.

Convair B-58A-10-CF Hustler 59-2456 with weapons load. (U.S. Air Force)
Convair B-58A-10-CF Hustler 59-2456 with weapons load. (U.S. Air Force)

The Convair Division of General Dynamics built 116 B-58s at Forth Worth, Texas. The first XB-58 flew on 11 November 1956. Production aircraft entered service with the Strategic Air Command in 1960 and were retired in 1970. Only eight aircraft remain in existence.

Convair B-58A strategic bombers in storage at Davis-Monthan Air Force Base, Tucson, Arizona. (Aviation Explorer)

¹ FAI Record File Number 4855

© 2018, Bryan R. Swopes

19 May 1976

Aviation, , , , ,
Captain James A. Yule, U.S. Air Force

19 May 1976: A Strategic Air Command Boeing B-52D Stratofortress eight-engine bomber took off from Carswell Air Force Base, Fort Worth, Texas on a training flight. As the airplane’s landing gear was retracting, the hydraulic system failed leaving the right front gear with its 2-wheel bogie partially retracted and unlocked. The hydraulic system failure also disabled the B-52’s steering, brakes and rudder. Captain James A. Yule, an Instructor Pilot, took command of the aircraft. SAC headquarters at Omaha, Nebraska, diverted the airplane to Edwards Air Force Base in California so that the bomber could land on the large dry lake bed there.

Rogers Dry Lake and Edwards Air Force Base, looking south west. Captain Yule landed his B-52 Stratofortress on the dry lake bed. (U.S. Air Force)
Rogers Dry Lake and Edwards Air Force Base, looking to the south west. Captain Yule landed his B-52 Stratofortress on the dry lake bed. The air base and its concrete runways are at the top center of the photograph. (U.S. Air Force)

After a five-hour flight and making several practice approaches, Captain Yule landed the aircraft. With no brakes, it coasted for two-and-a-half miles before coming to a stop. During the roll out, the right front bogie bounced up and down, providing no support. However, with the limited control available, Captain Yule successfully landed the Stratofortress with no damage and no injuries to the crew. He and another pilot received the Air Medal, and the rest of the air crew were awarded the Air Force Commendation Medal.

Boeing B-52D-75-BO Stratofortress 56-0606, the same type bomber flown by Captain James A. Yule, 19 May 1976. In this photograph, the airplane has its landing gear extended and flaps lowered. (U.S. Air Force)
Boeing B-52D-75-BO Stratofortress 56-0606, the same type bomber flown by Captain James A. Yule, 19 May 1976. In this photograph, the airplane has its landing gear extended and flaps lowered. (U.S. Air Force)

Captain Yule was the recipient of the Mackay Trophy for 1976. Established in 1911 and administered by the National Aeronautic Association, the Mackay Trophy is awarded to the “most meritorious flight of the year” by an Air Force person, persons, or organization. His citation reads:

The Mackay Trophy.
The Mackay Trophy.

“For gallantry and unusual presence of mind while participating in a flight as an instructor pilot of a B-52D Stratofortress.

“Captain James A Yule, distinguished himself by gallantry and unusual presence of mind while participating in an aerial flight as an instructor pilot of a B-52D aircraft on 19 May 1976. Captain Yule’s flight developed a unique multiple emergency and he assumed command of the aircraft, and at great personal risk, checked out the hydraulic open wheel well area to detect the problem. Using initiative, he coordinated with ground agencies and crew members and determined that a safe landing could be made after loss of braking and complete failure of steering. Captain Yule’s professional competence and outstanding airmanship under extreme stress resulted in successful recovery of the crew and a valuable aircraft. His courageous acts in landing a malfunctioning aircraft reflect great credit upon himself and the United States Air Force.”

© 2015, Bryan R. Swopes