Tag Archives: World Record For Speed Over a Closed Circuit Of 500 Kilometers

7 September 1961

Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)
Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)

7 September 1961: As a consultant to Northrop Corporation, Jackie Cochran flew a T-38A-30-NO Talon, 60-0551, to a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 500 Kilometers, flying from Edwards Air Force Base, California to Beatty, Nevada, Lone Pine, California, and back to Edwards. Her speed averaged 1,095.56 kilometers per hour (680.749 miles per hour).

Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)
Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)

Air Force test pilot Chuck Yeager kept notes during these record runs:

“September 7: Re-run 500 km. Good run. Observers miss her at Lone Pine, Calif.”

— Brigadier General Charles Elwood (“Chuck”) Yeager, U.S. Air Force, quoted in Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, Page 305.

During August and September 1961, Cochran set series of speed, altitude and distance records with the T-38.

The Northrop T-38A Talon is a two-place, twin-engine jet trainer capable of supersonic speed. It is 46 feet, 4 inches (14.122 meters) long with a wingspan of 25 feet, 3 inches (7.696 meters) and overall height of 12 feet, 10 inches (3.912 meters). The trainer’s empty weight is 7,200 pounds (3,266 kilograms) and the maximum takeoff weight is 12,093 pounds (5,485 kilograms).

The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. It is 108.1 inches (2.746 meters) long, 22.0 inches (0.559 meters) in diameter and weighs 584 pounds (265 kilograms).

It has a maximum speed of Mach 1.08 (822 miles per hour, 1,323 kilometers per hour) at Sea Level. The Talon’s service ceiling of 55,000 feet (16,764 meters) and it has a maximum range of 1,093 miles (1,759 kilometers).

In production from 1961 to 1972, Northrop has produced nearly 1,200 T-38s. As of January 2014, the U.S. Air Force had 546 T-38A Talons in the active inventory. It also remains in service with the U.S. Navy, and the National Aeronautics and Space Administration.

Jackie Cochran’s record-setting T-38 is in the collection of the Smithsonian Institution, National Air and Space Museum.

Northrop T-38A-30-NO Talon at Edwards Air Force Base, California. (U.S. Air Force)
Northrop T-38A-30-NO Talon 60-0551 at Edwards Air Force Base, California. (U.S. Air Force)

© 2017, Bryan R. Swopes

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3 September 1954

Major John L. Armstrong, U.S. Air Force, standing on the wing of his record-setting F-86H-1-NH  Sabre. (Jet Pilot Overseas)

3 September 1954: At the Dayton Air Show, being held for the first time at the James M. Cox Municipal Airport, Major John L. (“Jack”) Armstrong, U.S. Air Force, flew his North American Aviation F-86H-1-NH Sabre, 52-1998, to a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 500 Kilometers Without Payload, averaging 1,045.206 kilometers per hour (649.461 miles per hour).¹

Similar to the F-86H-1-NA Sabre flown by Captain Armstrong, this is F-86H-10-NH 53-1298. (U.S. Air Force)
Similar to the F-86H-1-NH Sabre flown by Captain Armstrong, this is F-86H-10-NH 53-1298. (U.S. Air Force)

The F-86H was a fighter-bomber variant of the famous Sabre Jet day fighter. It was equipped with a much more powerful General Electric J73-GE-3 turbojet engine. The engine was larger that the J47 used in previous F-86 models, and this required a much larger air intake and airframe modifications. The fuselage was 6 inches deeper and two feet longer than the F-86F. This accommodated the new engine and an increase in fuel load. The tail surfaces were changed with an increase in the height of the vertical fin and the elevators were changed to an “all-flying” horizontal stabilizer. The first F-86Hs built retained the six Browning AN-M3 .50 caliber machine guns of the F-86F, but this was quickly changed to four Pontiac M39 20 millimeter revolver cannon.

Another view of North American Aviation F-86-10-NH Sabre 53-1298. This fighter bomber i similar to the airplane flown by Colonel Armstrong to set a world speed record. (U.S. Air Force)
Another view of North American Aviation F-86-10-NH Sabre 53-1298. This fighter bomber is similar to the airplane flown by Major Armstrong to set a world speed record. (U.S. Air Force)

The North American Aviation F-86H Sabre was 38 feet, 10 inches (11.836 meters) long with a wingspan of 39 feet, 1 inch (11.913 meters) and overall height of 14 feet, 11 inches (4.547 meters). Empty weight was 13,836 pounds (6,276 kilograms) and gross weight was 24,296 pounds (11,021 kilograms).

The F-86H was powered by a General Electric J73-GE-3D or -3E engine, a single-spool, axial-flow, turbojet engine, which used a 12-stage compressor section with variable inlet vanes, 10 combustion chambers and 2-stage turbine section. It produced 8,920 pounds of thrust (39.68 kilonewtons) at 7,950 r.p.m. The J73 was 16 feet, 8 inches (5.08 meters) long, 3 feet, 3.5 inches (1.03 meters) in diameter and weighed 3,650 pounds (1,656 kilograms).

The F-86H had a maximum speed of 692 miles per hour (1,114 kilometers per hour) at Sea Level and 617 miles per hour (993 kilometers) at 30,000 feet (9,144 meters). The fighter bomber had an initial rate of climb of 12,900 feet per minute (65.53 meters per second) and it could reach 30,000 feet in 5.7 minutes. The service ceiling was 50,800 feet (15,484 meters). With bombs, the F-86H had a combat radius of 403 miles (649 kilometers) at 552 miles per hour (888 kilometers per hour). The maximum ferry range was 1,810 miles (2,913 kilometers).

F-86H Sabres (after the first ten production airplanes) were armed with four Pontiac M39 20 mm autocannon with 600 rounds of ammunition. In ground attack configuration, they could carry rockets and bombs or “Special Store” that would be delivered by “toss bombing.” 473 F-86H Sabres were built before production ended.

The F-86H Sabre became operational in 1954, but by 1958 all that remained in the U.S. Air Force Inventory were reassigned to the Air National Guard. The last one was retired in 1972.

North American Aviation F-86H Sabre. (U.S. Air Force)

John L. Armstrong was born in Orange County, California, 19 July 1922. He was the fourth child of Milton Williams Armstrong, an engineer, and Olive M. Meyer Armstrong. As a child, he was called “Jake.”

Major Armstrong had been a fighter pilot during World War II, flying Lockheed P-38 Lightnings, initially with the 554 Fighter Training Squadron, 496th Fighter Training Group.

On 13 March 1944, Armstrong made a forced landing at North Killingholme when his fighter ran out of fuel.

2nd Lieutenant Armstrong was assigned to the 79th Fighter Squadron, 20th Fighter Group based at RAF Kings Cliffe, Northamptonshire, England, 26 March 1944. He flew the Lockheed P-38 Lightning.

Lt. John L. Armstrong, 79th Fighter Squadron, 20th Fighter Group, with a Lockheed P-38 Lightning,1944. (The 20th Fighter Group Project)

The 79th transitioned to the P-51 Mustang. Armstrong was promoted to first lieutenant 26 June 1944. He was officially credited with having destroyed one enemy Focke-Wulf Fw 190. On 28 August 1944, while flying his 30th combat mission, his North American Aviation P-51D-5-NA Mustang, 44-13791, Guardian Angel,  was shot down by anti-aircraft gunfire while he was attacking a railway roundhouse at Bad Greuznach, Germany. Armstrong bailed out but was captured and held at Stalag Luft I at Barth, Western Pomerania. He was returned to U.S. military control in June 1945.

Major Armstrong had been awarded the Distinguished Flying Cross, the Air Medal with five oak leaf clusters (six awards), the Purple Heart, the Prisoner of War Medal, World War II Victory Medal, and the European-African-Middle Eastern Campaign Medal.

Two days after setting the speed record, Jack Armstrong was attempting to increase it. His Sabre broke up in flight and Major Armstrong was killed. His remains were buried at the Loma Vista Memorial Park, Fullerton, California, 11 September 1954.

This exhibit at the National Museum of the United States Air Force, Wright-Patterson AFB, ohio, commemorates Major Armstrong's record-setting flight. His flight helmet is included in the display. (U.S. Air Force)
This exhibit at the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio, commemorates Major Armstrong’s record-setting flight. His flight helmet is included in the display. Visible behind the display case is North American Aviation F-86H-10-NH Sabre 53-1352.  (U.S. Air Force)

¹ FAI Record File Number 8860

© 2017, Bryan R. Swopes

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23 May 1953

Jackie Cochran in cockpit of the Sabre Mk.3, with Major Charles E. Yeager, U.S. Air Force
Jackie Cochran in cockpit of the Canadair Sabre Mk.3, with Major Charles E. Yeager, U.S. Air Force (Air Force Flight Test Center History Office, U.S. Air Force)

23 May 1953: At Edwards Air Force Base, California, Jackie Cochran set another Fédération Aéronautique Internationale (FAI) speed record with the Canadair CL-13 Sabre Mk.3, No. 19200. Flying over a 500-kilometer closed circuit without payload, the Orenda-powered Sabre averaged 952.032 kilometers per hour (591.565 miles per hour).¹

“The following week a morning opened up with conditions satisfactory, except for a fifteen-knot wind, and I went around the course five times for a 500-kilometer record of 590 miles per hour. The plane, without the  carrying of external tanks, had fuel for only seventeen minutes of full-power low-altitude flying, so for this longer run I had to carry the external tanks, which slowed the airplane down by about 40 miles per hour. Even so, I only had fuel for twenty-seven minutes of full-power flying, which was insufficient, so I had to make the runs pulling 94 per cent of full power rather than full power. I landed on the dry lake bed just as I did after the 100-kilometer run and again with two minutes of fuel remaining.”

The Stars at Noon, by Jacqueline Cochran, Little, Brown and Company, Boston, 1954, Chapter XII, at Pages 230–231.

ackie Cochran’s FAI Diplome de Record at the San Diego Air and Space Museum Archives. (© 2015, Bryan R. Swopes)
Jackie Cochran’s FAI Diplôme de Record at the San Diego Air and Space Museum Archives. (© 2015, Bryan R. Swopes)

During May and June 1953, Cochran, a consultant to Canadair, flew the Sabre Mk.3 to FAI records over the 15/25 kilometer straight course, the 100-kilometer closed circuit, the 500-kilometer closed circuit and to an altitude record of 14,377 meters (47,168.635 feet). She was the first woman to “break the Sound Barrier” when she flew No. 19200 to Mach 1.04.

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 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.

Record-setting Canadair CL-13 Sabre Mk.3, No. 19200 (Canadair Ltd.)

¹ FAI Record File Number 9075

© 2017, Bryan R. Swopes

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1 May 1965

Lockheed YF-12A 60-6936, flies test mission near Edwards Air Force Base, Califrnia. (U.S. Air Force)
Lockheed YF-12A 60-6936, flies test mission near Edwards Air Force Base, Califrnia. (U.S. Air Force)

1 May 1965: Lockheed YF-12A 60-6936 established five Fédération Aéronautique Internationale (FAI) World Records for Speed: 3,351.507 kilometers per hour (2,070.102 m.p.h.) over a 15/25 Kilometer Straight Course; 2,644.22 kilometers per hour (1,643.04 miles per hour) over a 500 Kilometer Closed Circuit; and 2,718.01 kilometers per hour (1,688.89 miles per hour) over a 1,000 Kilometer Closed Circuit. On the same day, 6936 set an FAI World Record for Altitude in Horizontal Flight of 24,463 meters (80,259 feet).

The World Record-setting flight crews, from left to right, Captain James P. Cooney, Major Walter F. Daniel, Colonel Robert L. Stephens, Lieutenant Colonel Daniel Andre and Major Neil T. Warner. (U.S. Air Force)
The World Record-setting flight crews, from left to right, Captain James P. Cooney, Major Walter F. Daniel, Colonel Robert L. Stephens, Lieutenant Colonel Daniel Andre and Major Neil T. Warner. (U.S. Air Force)

The YF-12A interceptor prototype was flown by pilots Major Walter F. Daniel and Colonel Robert L. Stephens, with fire control officers Lieutenant Colonel Daniel Andre, Major Neil T. Warner and Captain James P. Cooney. Colonel Stephens and Lieutenant Colonel Andre were awarded the Thompson Trophy for the “J” Division, 1965. Their trophy is in the collection of the National Museum of the United States Air Force.

Lockheed YF-12A 60-6936 during speed record trials. The white cross on the aircraft's belly was to assist timers and observers. (U.S. Air Force)
Lockheed YF-12A 60-6936 taking off from Edwards Air Force Base during the speed record trials, 1 May 1965. The white cross on the aircraft’s belly was to assist timers and observers. (U.S. Air Force)

FAI Record File Num #3972 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km with 1 000 kg payload
Performance: 2 718.01 km/h
Date: 1965-05-01
Course/Location: Edwards AFB, CA (USA)
Claimant Walter F. Daniel (USA)
Aeroplane: Lockheed YF-12A (06936)
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #3973 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km with 2 000 kg payload
Performance: 2 718.01 km/h
Date: 1965-05-01
Course/Location: Edwards AFB, CA (USA)
Claimant Walter F. Daniel (USA)
Aeroplane: Lockheed YF-12A (06936)
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #8534 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Altitude in horizontal flight
Performance: 24 463 m
Date: 1965-05-01
Course/Location: Edwards AFB, CA (USA)
Claimant R.L. Stephens (USA)
Aeroplane: Lockheed YF-12A
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #8855 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 500 km without payload
Performance: 2 644.22 km/h
Date: 1965-05-01
Course/Location: Edwards AFB, CA (USA)
Claimant Walter F. Daniel (USA)
Aeroplane: Lockheed YF-12A
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #8926 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km without payload
Performance: 2 718.006 km/h
Date: 1965-05-01
Course/Location: Edwards AFB, CA (USA)
Claimant Walter F. Daniel (USA)
Aeroplane: Lockheed YF-12A
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #9059 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a straight 15/25 km course
Performance: 3 331.507 km/h
Date: 1965-05-01
Course/Location: Edwards AFB, CA (USA)
Claimant R.L. Stephens (USA)
Aeroplane: Lockheed YF-12A
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

World Speed Record holders and Thompson Trophy winners, Colonel Robert F. Stephens and Lieutenant Colonel Daniel Andre. (U.S. Air force)
World Speed Record holders and Thompson Trophy winners, Colonel Robert L. Stephens and Lieutenant Colonel Daniel Andre. (U.S. Air Force)

60-6936 was one of three Mach 3 YF-12A interceptors designed and built by Kelly Johnson’s “Skunk Works”. It was developed from the CIA’s Top Secret A-12 Oxcart reconnaissance airplane. The YF-12A was briefly known as the A-11, which was a cover story to hide the existence of the A-12. Only three were built. The Air Force ordered 93 F-12B interceptors into production as a replacement for the Convair F-106A Delta Dart, but for three straight years Secretary of Defense Robert S. McNamara refused to release the funds that had been appropriated. In 1968, the F-12B project was cancelled.

On 24 June 1971, 60-6936 suffered an in-flight fire while on approach to Edwards Air Force Base. The crew successfully ejected and the airplane crashed a few miles to the north of EDW. It was totally destroyed.

The only surviving example of a YF-12A, 60-6935, is in the collection of the National Museum of the United States Air Force.

The 1965 Thompson Trophy on display at the National Museum of the United States Air Force. (U.S. Air Force)
The 1965 Thompson Trophy on display at the National Museum of the United States Air Force. (U.S. Air Force)

© 2016, Bryan R. Swopes

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15 April 1959

This McDonnell RF-101C-60-MC Voodoo, 56-055, is the sister ship of the Voodoo flown by Captain Edwards to set a World Speed Record, 15 April 1959. (Unattributed)
This McDonnell RF-101C-60-MC Voodoo, 56-055, is the sister ship of the airplane flown by Captain Edwards to set a World Speed Record, 15 April 1959. (Hervé Cariou)
Captain George A. Edwards, Jr., in teh cockpit of his McDonnell RF-101C Voodoo, after setting an FAI World Record for Speed. (U.S. Air Force)
Captain George A. Edwards, Jr., in the cockpit of his McDonnell RF-101C Voodoo, after setting an FAI World Record for Speed. (U.S. Air Force)

15 April 1959: Captain George A. Edwards, Jr., United States Air Force, assigned to the 432nd Tactical Reconnaissance Wing, Shaw Air Force Base, South Carolina, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 500 Kilometers (310.686 miles) Without Payload at Edwards Air Force Base, California. Captain Edwards flew a McDonnell RF-101C-60-MC Voodoo, serial number 56-054. His speed over the course averaged 1,313.677 kilometers per hour (816.281 miles per hour).¹

Captain Edwards told The Nashville Tennessean, “The flight was routine. The plane ran like a scalded dog.”

Nine days earlier, Colonel Edward H. Taylor flew another McDonnell RF-101C to a World Record for Speed Over a 1000 Kilometer Course of 1,126.62 kilometers per hour (700.05 miles per hour).²

McDonnell RF-101C-65-MC Voodoo 56-068, very similar to the aircraft flown by Captain Edwards. (U.S. Air Force)
McDonnell RF-101C-65-MC Voodoo 56-068, of the 363rd Tactical Reconniassance Wing, Shaw AFB, is very similar to the Voodoo flown by Captain Edwards. 15 April 1969. (U.S. Air Force)

George Allie Edwards, Jr., was born in Nashville, Tennessee in 1929, the son of George Allie Edwards, an automobile agent, and Veriar (“Vera”) Lenier Edwards. When his father died, his mother, younger sister Jane, and George went to live with Mrs. Edwards’ parents at Crossville, Tennessee. He attended Cumberland High School and studied at the University of Tennessee. He took flight lessons at the age of 15 and accumulated more than 2,000 flight hours over the next six years.

In 1951, during the Korean War, Edwards entered the United States Air Force as an aviation cadet. He graduated from flight school at Vance Air Force Base, Oklahoma, and was commissioned a second lieutenant. He was assigned to the 67th Tactical Reconnaissance Wing at Kimpo Air Base, South Korea. As a pilot of North American RF-51D Mustang and Lockheed RF-80 Shooting Star photographic reconnaissance airplanes, he flew 101 combat missions.

His next assignment was as a jet instructor at Bryan Air Force Base, Texas, and then an F-100 pilot with the 354th Tactical fighter Wing, and then served as chief of safety and standardization for the 432nd Tactical Reconnaissance Wing. It was during this assignment that he set the world record.

Major George A. Edwards climbs to the cockpit of a McDonnell RF-4C Phantom II. (Lake Travis View)
Lieutenant Colonel George A. Edwards climbs to the cockpit of a McDonnell RF-4C Phantom II. (Lake Travis View)

From 1959 to 1962, Edwards was an advisor to the West German Air Force. In recognition for his service, the chief of staff awarded him Luftwaffe pilot’s wings. For the next several years, he rotated through a series of training assignments, education and staff assignments.

During the Vietnam War, Lieutenant Colonel Edwards commanded the 19th Tactical Reconnaissance Squadron which was equipped with the McDonnell RF-4C Phantom II reconnaissance variant. He also commanded a detachment of the 460th Tactical Reconnaissance Wing, and flew the Martin RB-57 Canberra. Edwards flew another 213 combat missions.

Colonel Edwards went on to command the 67th Tactical Reconnaissance Wing, (which he had previously served with during the Korean War), Bergstom Air Force Base, Texas; as a brigadier general, was vice commander of 12th Air Force; commander 314th Air Division, Osan Air Base, Republic of Korea, and also commanded the Korean Air Defense Sector. Edwards was promoted to Major General 1 August 1976, with an effective date of rank of 1 July 1973.

Major General George A. Edwards, Jr., United States Air Force.

During his career in the United States Air Force, Major General George A. Edwards, Jr., was awarded the Distinguished Service Medal, Legion of Merit, Distinguished Flying Cross with four oak leaf clusters (5 awards), the Bronze Star, Air Medal with 19 oak leaf clusters (20 awards), Joint Service Commendation Medal, Air Force Commendation Medal, Presidential Unit Citation emblem, Air Force Outstanding Unit Award ribbon with four oak leaf clusters (5 awards).

General Edwards retired from the Air Force 1 March 1984 after 33 years of service. As of 2015, the General and Mrs. Edwards live near Austin, Texas.

McDonnell RF-101C Voodoo 56-042, 15th Tactical Reconnaissance Squadron. (U.S. Air Force)
McDonnell RF-101C-60-MC Voodoo 56-042, 15th Tactical Reconnaissance Squadron. (U.S. Air Force)

The RF-101C Voodoo was an unarmed reconnaissance variant of the F-101C fighter. It was 69 feet, 4 inches (21.133 meters) long with a wingspan of 39 feet, 8 inches (12.090 meters). The height was 18 feet (5.486 meters). Empty weight for the RF-101C was 26,136 pounds (11,855 kilograms), with a maximum takeoff weight of 51,000 pounds (23,133 kilograms).

Two Pratt & Whitney J57-P-13 turbojet engines. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor (9 low- and 7 high-pressure stages), 8 combustors and a 3-stage turbine (1 high- and 2 low-pressure stages). The J57-P-13 was rated at 10,200 pounds of thrust (45.37 kilonewtons), and 15,800 pounds (70.28 kilonewtons) with afterburner.

The aircraft had a maximum speed of 1,012 miles per hour (1,629 kilometers per hour) at 35,000 feet (10,668 meters). The service ceiling was 55,300 feet (16,855 meters). The Voodoo could carry up to three drop tanks, giving a total fuel capacity of 3,150 gallons (11,294 liters) and a maximum range of 2,145 miles (3,452 kilometers).

The RF-101C carried six cameras in its nose. Two Fairchild KA-1s were aimed downward, with four KA-2s facing forward, down and to each side.

Beginning in 1954, McDonnell Aircraft Corporation built 807 F-101 Voodoos. 166 of these were the RF-101C variant. This was the only F-101 Voodoo variant to be used in combat during the Vietnam War. The RF-101C remained in service with the U.S. Air Force until 1979.

This McDonnell RF-101C-45-Voodoo, 56-0183, of the 20th Tactical Reconnaissance Squadron, is similar in appearance to the Voodoo flown by Captain Edwards, 15 April 1959. (Unattributed.
This McDonnell RF-101C-45-Voodoo, 56-0183, of the 20th Tactical Reconnaissance Squadron, 432nd Tactical Reconnaissance Wing, is similar in appearance to the Voodoo flown by Captain Edwards, 15 April 1959. (Unattributed)

¹ FAI Record File Number 8858

² FAI Record File Number 8928

© 2017, Bryan R. Swopes

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