Major John H. Glenn, Jr., U.S. Marine Corps, in the cockpit of his North American Aviation F-86F Sabre, “MiG Mad Marine,” just after his second kill, 19 July 1953.
23 July 1953: Major John H. Glenn, Jr., United States Marine Corps, shot down his third and final MiG-15 fighter during the Korean War.
Major Glenn had previously flown a Grumman F9F Panther with VMF-311, but was assigned to the U.S. Air Force 25th Fighter Interceptor Squadron, 51st Fighter Interceptor Group, at K13, Suwon, Korea.
Major John H. Glenn, Jr., United States Marine Corps, standing with his North American Aviation F-86-30-NA Sabre, 52-4584, “MiG Mad Marine,” at Suwon, Korea, July 1953. (John Glenn Archives, The Ohio State University)
While on temporary duty with the Air Force squadron, Glenn flew the North American Aviation F-86F Sabre air superiority fighter. He shot down all three MiG fighters with F-86F-30-NA serial number 52-4584. His previous victories were on 12 July and 19 July, 1953, also against MiG-15 fighters.
Major Glenn had painted the names of his wife and two children, “Lyn Annie Dave,” on the nose of his airplane, but after being heard complaining that there “weren’t enough MiGs,” he came out one morning to find MIG MAD MARINE painted on the Sabre’s side.
John Glenn’s fighter, North American Aviation F-86F-30-NA Sabre, serial number 52-4584, at K13, Suwon, Korea, 1953. (U.S. Air Force)
Joe Walker with the Number 2 North American Aviation X-15A, 56-6671, on Rogers Dry Lake. (NASA)Joseph A. Walker, NASA Chief Research Test Pilot
19 July 1963: Between 1960 and 1963, NASA Chief Research Test Pilot Joseph Albert Walker made 25 flights in the North American Aviation X-15A hypersonic research rocketplanes. His 24th flight was the 21st for the Number 3 X-15, 56-6672, and the 90th of the X-15 program.
At 10:20:05.0 a.m., Walker and the X-15 were airdropped from the Boeing NB-52B Stratofortress, 53-008, Balls 8, over Smith Ranch Dry Lake, Nevada. Walker fired the Reaction Motors XLR99-RM-1 rocket engine and over the next 84.6 seconds the engine’s 60,000 pounds of thrust drove the X-15 upward. The engine’s thrust on this flight was higher than expected, shutdown was 1.6 seconds late, and Walker’s climb angle was 1½° too high, so the X-15 overshot the predicted maximum altitude and its ballistic arc peaked at 347,800 feet (106,010 meters, 65.8 miles). The maximum speed was Mach 5.50 (3,714 miles per hour, 5,977 kilometers per hour).
Walker glided to a touch down at Rogers Dry Lake, Edwards Air Force Base California, after flying 311 miles in 11 minutes, 24.1 seconds of flight. On this flight, Joe Walker became the first American civilian to fly into Space.
North American Aviation X-15A 56-6672 on Rogers Dry Lake after a flight. (NASA)
LCOL William F. Barns with his North American Aviation F-86D-35-NA Sabre 51-6145, after his record-setting flight, 16 July 1953. (U.S. Air Force)
16 July 1953: Lieutenant Colonel William F. Barns, United States Air Force, set a Fédération Aéronautique Internationale (FAI) absolute World Record for Speed Over a 3 Kilometer Straight Course at the low-altitude course at the Salton Sea, California. ¹
Colonel Barns flew this North American Aviation F-86D-35-NA Sabre, serial number 51-6145, a radar-equipped all-weather interceptor. Lieutenant Colonel Barns was the Air Material Command’s pilot representative at the North American Aviation Los Angeles plant. The Sabre was a standard production airplane, the first Block 35 model built. It was fully loaded with twenty-four 2.75-inch (70 millimeter) aerial rockets.
Barns made the FAI-required four passes—two in each direction—in the Sabre interceptor. His four passes were timed at 720.574, 710.515, 721.351, and 710.350 miles per hour. (1,159.651, 1,143.463, 1,160.902, and 1,143.198 kilometers per hour).
Lieutenant Colonel William F. Barns, the Air Material Command’s pilot representative at the North American Aviation Los Angeles plant, in the cockpit of a brand-new North American Aviation F-86D-30-NA Sabre, 51-6112. (Jet Pilot Overseas)
Barns averaged 715.745 miles per hour (1,151.88 kilometers per hour) at only 125 feet (38 meters) above the surface. The air temperature was 105 °F. (40.5 °C.)
The surface of the Salton Sea is -236 feet (-71.9 meters)—below Sea Level. Barns’ Sabre was flying at -111 feet (-33.8 meters). Under these conditions, the speed of sound, Mach 1, was 794 miles per hour (1,278 kilometers per hour), so the margin between the record speed and the onset of transonic compressibility effects was increased. Barns’ Sabre reached a maximum 0.91 Mach under these conditions.
North American Aviation F-86D-35-NA Sabre 51-6145, FAI World Speed Record holder.
The Associated Press reported the event:
Air Force Colonel Breaks Record
THERMAL, Calif. (AP)—An Air Force colonel flashed to a new air speed record of 715.7 miles per hour Thursday in a north American F-86D Sabre Jet.
Skimming over the hot beach of Southern California’s Salton Sea, Lt. Col. William F. Barns, 32, broke the record set last Nov. 19 over the same run by Capt. J. Slade Nash of Edwards Air Force Base.
On his first try, Barns averaged 713.6 miles per hour, a record performance, but came back a half hour later to beat that.
The airplane could not exceed 500 meters altitude (1,640 feet) at any time after takeoff on the trial, and the 3-kilometer dash had to be made below 100 meters (328 feet).
—The Daily Illini, 17 July 1953, Vol. 82, Number 189, at Page 1, Column 2.
The same F-86D, 51-6145, flown by Captain Harold E. Collins, set an FAI World Record for Speed Over a 15/25 Kilometer Straight Course of 1,139.219 kilometers per hour (707.878 miles per hour) at Vandalia. Ohio, 1 September 1953. ²
William Frederick Barns was born 30 August 1920 at Baltimore, Maryland. He was the son of Claude Cox Barns and Nellie C. Hedrick Barns. The family moved to the Hawaiian Islands in 1925. He attended Theordore Roosevelt High School, in Honolulu. In 1940, William was employed as a clerk at the Bishop National Bank.
Barns began civilian flight training at John Rodgers Field near Honolulu in 1941, and was at the airfield during the attack on the Hawaiian Islands by the Imperial Japanese Navy, 7 December 1941. Barns enlisted in U.S. Army Air Corps 13 April 1942. He had brown hair and eyes, was 5 feet, 10 inches (1.78 meters) tall, and weighed 138 pounds. After qualifying as a pilot at Luke Field, Arizona, Barns was commissioned as a second lieutenant, U.S. Army Air Forces.
During World War II, Barns flew 210 combat missions with the 324th Fighter Group. He was awarded the Distinguished Flying Cross and the Silver Star.
Major and Mrs. William F. Barns, Honolulu, Oahu, Hawaiian Islands, 1949.
Colonel Barns married Miss Marylouise Hamilton at the Flyer’s Chapel of the Mission Inn, Riverside, California, 18 August 1947. They had two children, Terrie and Bill. At the time of Barn’s world speed record, the family resided in Palos Verdes Estates, a few miles south of the North American factory.
Colonel Barns retired from the U.S. Air Force, 31 May 1966. He died in Phoenix, Arizona, 17 April 1995.
North American Aviation F-86D-1-NA Sabre 50-463. (North American Aviation, Inc.)
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 radar and armed with twenty-four unguided 2.75-inch (69.85 millimeter) diameter Mark 4 Folding-Fin Aerial Rockets (FFAR) carried in a retractable tray in its belly.
A North American Aviation, Inc. advertisement, 1953. (Vintage Ad Browser)
The aircraft was so complex that the pilot training course was the longest of any aircraft in the U.S. Air Force inventory, including that of the Boeing B-47 Stratojet.
The F-86D was larger than the F-86A, E and F fighters, with a wider fuselage. Its length was increased to 40 feet, 3 inches (12.268 meters) with a wingspan of 37 feet, 1.5 inches (11.316 meters), and its height is 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).
North American Aviation F-86D-20-NA Sabre 51-3045. (U.S. Air Force)
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).
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.
North American Aviation F-86D-60-NA Sabre 53-4061 firing a salvo of FFARs.
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.
A potential adversary of the North American Aviation F-86D Sabre all-weather interceptor was the Tupolev Tu-85 long-range strategic bomber.
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 world-record-setting Sabre, 51-6145, was transferred to NATO ally, the Royal Hellenic Air Force.
North American Aviation F-86D-30-NA Sabre 51-6143, right roll over Malibu, California.
29 June 1965: At 10:21:17.6 PDT, Captain Joe H. Engle, United States Air Force, flying the Number Three North American Aviation X-15A-3 research rocketplane, 56-6672, was air-dropped from the NB-52B Stratofortress mothership, Balls 8, over Delamar Dry Lake in Nevada. This was the 138th flight of the X-15 Program, and Joe Engle’s 12th. He fired the Reaction Motors XLR99-RM-1 engine for 81.0 seconds and accelerated to Mach 4.94 (3,432 miles per hour, 5,523 kilometers per hour). The X-15 climbed to an altitude of 280,600 feet (85,527 meters, 53.14 miles). He touched down at Edwards Air Force Base after 10 minutes, 34.2 seconds of flight. His parents were at Edwards to witness his flight.
Captain Engle qualified for Astronaut wings on this flight, the third and youngest Air Force pilot to do so.
Command Pilot Astronaut insignia, United States Air Force
From 1963 and 1965, Joe Engle made 14 flights in the three X-15s. After leaving the X-15 Program, he was assigned to the Apollo Program, the only NASA astronaut with prior spaceflight experience. He was the back-up Lunar Module pilot for Apollo 14 and he was the designated LM pilot for Apollo 17 but was replaced by Harrison Schmidt when Apollo 18 was cancelled. Next he went on to the Space Shuttle Program. He was a Mission Commander for the Enterprise flight tests and for Columbia‘s second orbital flight, during which he became the only pilot to manually fly a Mach 25 approach and landing. Finally, he commanded the Discovery STS 51-1 mission.
Joe Engle retired from the Air Force in 1986. He was then promoted to the rank of Major General and assigned to the Kansas Air National Guard. He has flown at least 185 aircraft types and accumulated 14,700 flight hours, with 224 hours in space.
Captain Joe H. Engle, U.S. Air Force, with the North American Aviation X-15A-2, 56-6671, at Edwards Air Force Base, California, 1965. (NASA)
North American Aviation Engineering Test Pilot Louis Wait with a wind tunnel model of the NA-73X. (North American Aviation, Inc.)
28 June 1940: A ¼–scale mahogany model of the North American Aviation NA-73X, prototype of the Royal Air Force Mustang Mk.1, was tested in the Ten-Foot Wind Tunnel at the Guggenheim Aeronautical Laboratory of the California Institute of Technology (GALCIT) in Pasadena, California, from 28 June to 26 July 1940.
The Ten-Foot Tunnel was funded by a $300,000 grant from the Daniel Guggenheim Foundation. Construction of the Laboratory began in 1927 and the wind tunnel became operational in November 1929. A 15 foot (4.572 meter) diameter fan was capable of producing air speeds up to 200 miles per hour (322 kilometers per hour). The first complete scale model airplane to be tested was the Northrop Alpha.
Airships, airplanes, and structures (bridges, buildings) were tested in the tunnel. According to Caltech, the Douglas Aircraft Company used the facility more than any other manufacturer.
During World War II, a staff of sixty worked three shifts, seven days a week. A technician who worked there later said, “We had a tighter schedule than the tightest schedule anyone ever had.”
The wind tunnel’s test equipment was damaged by the Whittier Narrows Earthquake. It was closed in 1997 to be replaced by a new facility.
Model builders working on a scale model wing for use in NACA’s wind tunnels. (NASA)
