24 January 1962: The McDonnell Aircraft Corporation delivered the first F-110A Spectre to Colonel Gordon Graham and Colonel George Laven, United States Air Force, at the McDonnell plant at St. Louis, Missouri. The F-110A was soon redesignated as the F-4C Phantom II.
Two Phantoms were delivered to the Air Force for evaluation at Langley Field, Virginia. They were U.S. Navy F4H-1 Phantom IIs, Bureau of Aeronautics serial numbers 149405 and 149406. Initially the aircraft retained the Navy serial numbers but eventually were assigned Air Force numbers 62-12168 and 62-12169. The Air Force bailed them back to McDonnell to develop the YF-4C prototypes.
62-12169 (ex-Bu. No. 149406) was converted to a JF-4B (a special test aircraft). Operated by the McDonnell-Douglas Aircraft Center at Holloman Air Force Base, New Mexico, it suffered an engine explosion, 8 March 1967. McDonnell test pilot Charles (“Pete”) Garrison successfully ejected. The airplane crashed and was destroyed.
McDonnell built 5,057 Phantom IIs. They served with the United States Navy and Marine Corps, the U.S. Air Force, and many allied nations. The last Phantom II, an F-4E, was completed 25 October 1979. The U.S. Air Force retired its last operational Phantoms from service 20 December 2004, 42 years, 10 months, 27 days after receiving the first F-110A.
8 January 1973: Captain Paul D. Howman and First Lieutenant Lawrence W. Kullman, 4th Tactical Fighter Squadron, 432d Tactical Reconnaissance Wing, flying McDonnell F-4D-29-MC Phantom II 65-0796, were leading a flight of two fighters on combat air patrol in Route Pack III. Their call sign was CRAFTY ONE. A U.S. Navy guided missile cruiser, call sign RED CROWN, was steaming in the Gulf of Tonkin off the coast of North Vietnam, providing radar coverage for the fighters.
The following is a recount of the last USAF MiG kill in Southeast Asia; it occurred on 8 January 1973.
Crafty, a flight of two F-4s from the 4th Tactical Fighter Squadron, was assigned a night MiGCAP mission in support of B-52 strikes. They ingressed North Vietnam through the “Gorilla’s Head” and established their CAP about 70 miles southwest of Hanoi. The pilot of Crafty One was Captain Paul D. Howman. His backseater was First Lieutenant Lawrence W. Kullman. The following is Captain Howman’s description of the kill.
“About five minutes after arriving on station, we were advised by Red Crown that a MiG was airborne out of Phuc Yen and was heading southwest toward the inbound strike force. They vectored us northwest and told us he had leveled at 13,000 feet. Passing through [a heading of] north, we picked him up on radar at about 60 miles. We were able to follow him most of the way in as the range decreased. At about 30 miles, I called 02 and we jettisoned our centerline tanks.”
Crafty One and Two descended to 12,000 feet at 400 knots, still taking vectors. Red Crown turned them to a northeasterly heading. At 16 miles, Red Crown cleared Crafty to fire. Captain Howman’s account continues.
“At 10 miles I got a visual on an afterburner plume 20 degrees right and slightly high. I called him out to the backseater and put the pipper on him. At 6 miles Lt. Kullman got a good full-system radar lock-on. Range was about 4 miles and overtake 900+ knots when I squeezed the trigger. The missile came off, did a little roll to the left, and tracked toward the “burner plume.” It detonated 50 feet short of his tail.
“I squeezed another one off at 2 miles range. This one just pulled some lead, then went straight for the MiG. It hit him in the fuselage and the airplane exploded and broke into three big flaming pieces.”
After determining there were no more MiGs in the area, Crafty returned to orbit for their remaining CAP period. They returned to base without further incident.
—The Tale of Two Bridges ; and The Battle for the Skies Over North Vietnam, by Major A. J. C. Lavalle, USAF, editor, Office of Air Force History, Washington, D.C., 1985, Chapter VI at Page 187–188.
The MiG 21 that Howman and Kullman shot down was the last air-to-air victory by the United States Air Force during the Vietnam War. Both men were awarded the Silver Star.
Their airplane, 65-0796, served another seventeen years before being retired. Today, it is on display at William E. Dyess Elementary School, Abilene, Texas.
2 January 1967: This painting, MiG Sweep, by aviation artist Keith Ferris, depicts “Olds 01” during OPERATION BOLO. The twin-engine all-weather jet fighter, a McDonnell F-4C -21-MC Phantom II, serial number 63-7680, was flown by Colonel Robin Olds, USAF, with First Lieutenant Charles C. Clifton, USAF, as the Weapons System Operator.
In this painting by Keith Ferris, the Phantom is shown inverted as Colonel Olds maneuvers to fire an AIM-9B Sidewinder heat-seeking missile at a North Vietnamese Mikoyan-Gurevich MiG-21 over Hanoi. Robin Olds was the only U.S. Air Force ace with victories in both World War II and Vietnam.
The area around Hanoi, North Vietnam, was the most heavily defended target area ever encountered by the United States Air Force. A combination of radar-directed anti-aircraft artillery, surface-to-air guided missiles, and fighter interceptors made every mission very dangerous. Republic F-105 Thunderchief fighter bombers were taking heavy losses to the Soviet-built Mikoyan-Gurevich MiG-21PFL fighters. When escorting F-4C Phantoms would try to engage the MiGs, they would return to their bases which were safe from attack under the American rules of engagement.
OPERATION BOLO was a complex plan to lure the ground-controlled MiG 21s into an air battle by having the Phantoms simulate a Thunderchief attack. Colonel Olds led 48 McDonnell F-4Cs of the 8th and 366th Tactical Fighter Wings on the same type of attack that would have been used by the Thunderchiefs, but rather than carrying a full load of bombs, the F-4s were armed with AIM-7E Sparrow radar-guided missiles and AIM-9B Sidewinder heat-seeking missiles. (The F-4C was not armed with a gun.)
As the Mach 2+ MiG 21s started coming up through the clouds, their pilots quickly realized that instead of the vulnerable targets of F-105s on a bomb run, they were faced with air superiority fighters.
In the official after action report, Colonel Olds said,
“At the onset of this battle, the MiGs popped up out of the clouds. Unfortunately, the first one to pop through came up at my 6 o’clock position. I think this was more by chance than by design. As it turned out, within the next few moments, many others popped out of the clouds in varying positions around the clock.
“This one was just lucky. He was called out by the second flight that had entered the area, they were looking down on my flight and saw the MiG-21 appear. I broke left, turning just hard enough to throw off his deflection, waiting for my three and four men to slice in on him. At the same time I saw another MiG pop out of the clouds in a wide turn about my 11 o’clock position, a mile and a half away. I went after him and ignored the one behind me. I fired missiles at him just as he disappeared into the clouds.
“I’d seen another pop out in my 10 o’clock position, going from my right to left; in other words, just about across the circle from me. When the first MiG I fired at disappeared, I slammed full afterburner and pulled in hard to gain position on this second MiG. I pulled the nose up high about 45 degrees, inside his circle. Mind you, he was turning around to the left so I pulled the nose up high and rolled to the right. This is known as a vector roll. I got on top of him and half upside down, hung there, and waited for him to complete more of his turn and I timed it so that as I continued to roll down behind him, I’d be about 20 degrees angle off and about 4,500 to 5,000 feet behind him. That’s exactly what happened. Frankly, I’m not sure he ever saw me. When I got down low and behind, and he was outlined by the sun against a brilliant blue sky, I let him have two Sidewinders, one of which hit and blew his right wing off”
—Aces and Aerial Victories: The United States Air Force in Southeast Asia 1965–1973, by R. Frank Futrell, William H. Greenhalgh, Carl Grubb, Gerard E. Hasselwander, Robert F. Jakob and Charles A. Ravenstein, Office of Air Force History, Headquarters USAF, 1976, Chapter II at Page 39.
The F-4Cs succeeded in shooting down seven MiG 21s, with another two probably destroyed. This accounted for about half of the VPAF’s MiG 21 complement.
With another flight crew, the Phantom flown by Robin Olds on 2 January 1967, McDonnell F-4C-21-MC 63-7680, shot down a MiG 17 on 13 May 1967. It was itself shot down by antiaircraft fire while attacking a SAM site, 20 November 1967. The Weapons System Officer, 1st Lieutenant James L. Badley, bailed out and was rescued, but the pilot, Captain John M. Martin, was not seen to leave the aircraft and is listed as Missing in Action.
15 December 1965: At 13:37:26 UTC, Gemini 6A, with NASA astronauts Captain Walter M. Schirra, Jr., United States Navy and Major Thomas P. Stafford, United States Air Force, on board, lifted off from Launch Complex 19 at the Cape Kennedy Air Force Station, Cape Kennedy, Florida. During its fourth orbit, Gemini 6A rendezvoused with Gemini 7, carrying Major Frank F. Borman II, USAF, and LCDR James A. Lovell, Jr., USN.
This was the first time that two manned space vehicles had rendezvoused in Earth orbit.
The two spacecraft remained together for 5 hours, 19 minutes before separating to a distance of approximately 10 miles (16 kilometers).
Gemini 7 had been in orbit since 4 December. Gemini 6, then 6A, had been postponed several times before finally launching on 15 December. It would return to Earth the following day, landing in the North Atlantic Ocean. Gemini 7 remained in orbit until 18 December.
The two-man Gemini spacecraft was built by the McDonnell Aircraft Corporation of St. Louis, Missouri, the same company that built the earlier Mercury space capsule. The spacecraft consisted of a series of cone-shaped segments forming a reentry module and an adapter section. It had an overall length of 18 feet, 9.84 inches (5.736 meters) and a maximum diameter of 10 feet, 0.00 inches (3.048 meters) at the base of the equipment section. The reentry module was 11 feet (3.353 meters) long with a maximum diameter of 7 feet, 6.00 inches (2.347 meters). The Gemini re-entry heat shield was a spherical section with a radius of 12 feet, 0.00 inches (3.658 meters). The weight of the Gemini spacecraft varied from ship to ship. Gemini VII had a gross weight of 8,076.10 pounds (3,663.26 kilograms) at launch. It was shipped from St. Louis to Cape Kennedy in early October 1965.
The Titan II GLV was a “man-rated” variant of the Martin Marietta Corporation SM-68B intercontinental ballistic missile. It was assembled at Martin’s Middle River, Maryland, plant so as not to interfere with the production of the ICBM at Denver, Colorado. Twelve GLVs were ordered by the Air Force for the Gemini Program. The GLV-7 first and second stages were shipped from Middle River to Cape Kennedy on 9 October 1965.
The Titan II GLV was a two-stage, liquid-fueled rocket. The first stage was 70 feet, 2.31 inches (21.395 meters) long with a diameter of 10 feet (3.048 meters). It was powered by an Aerojet Engineering Corporation LR87-7 engine which combined two combustion chambers and exhaust nozzles with a single turbopump unit. The engine was fueled by Aerozine 50, a hypergolic 51/47/2 blend of hydrazine, unsymetrical-dimethyl hydrazine, and water. Ignition occurred spontaneously as the components were combined in the combustion chambers. The LR87-7 produced approximately 430,000 pounds of thrust (1,912.74 kilonewtons). It was not throttled and could not be shut down and restarted. Post flight analysis indicated that the first stage engine of GLV-7 had produced an average of 462,433 pounds of thrust (2,057.0 kilonewtons). The second stage was 25 feet, 6.375 inches (7.031 meters) long, with the same diameter, and used an Aerojet LR91 engine which produced approximately 100,000 pounds of thrust (444.82 kilonewtons), also burning Aerozine 50. GLV-7’s LR91 produced an average of 102,584 pounds of thrust (456.3 kilonewtons).
The Gemini/Titan II GLV-7 combination had a total height of 107 feet, 7.33 inches (32.795 meters) and weighed 346,228 pounds (157,046 kilograms) at ignition.
12 December 1957: Major Adrian Eason Drew, U.S. Air Force, commanding officer, 481st Fighter Bomber Squadron, 27th Fighter Bomber Wing, Tactical Air Command, set a new Fédération Aéronautique Internationale (FAI) absolute speed record over the 15/25 kilometer course at Edwards Air Force Base, California.¹ Major Drew flew a modified McDonnell F-101A-5-MC Voodoo, serial number 53-2426.
The Voodoo, the ninth production F-101A, had been bailed to Pratt & Whitney by the Air Force to test a new J57-P-55 afterburning turbojet engine intended for the F-101B Voodoo, and it was redesignated JF-101A. The new engine produced 16,000 pounds of thrust with afterburner. The modified aircraft had longer jet exhaust tubes, and air scoops were installed in the belly to provide additional cooling air for the afterburners.
At 39,000 feet (11,887 meters), Major Drew accelerated for 65 miles (105 kilometers) before entering the 10.1 statute mile (16.25 kilometers) course. He made one pass in each direction. Actual time on course, each way, was 29.8 seconds. The official average speed for the two passes is 1,943.5 kilometers per hour (1,207.64 miles per hour). Although the air temperature was -79 °F. (-62 °C.), frictional heating brought the Voodoo’s skin temperature to 190 °F. (88 °C.), high enough to blister the airplane’s paint.
Major Drew was awarded the Distinguished Flying Cross and the Thompson Trophy for 1957.
Adrian Eason Drew was born 8 October 1920 in Georgia, the first of six children of John Robert Drew, a farmer, and Ada Elma Eason Drew.
After one year of college, Adrian Drew enlisted as a private in the U.S. Army Air Corps, 31 March 1942, at Fort McClellan, Alabama. He was 5 feet, 8 inches (1.73 meters) tall and weighed 143 pounds (64.9 kilograms).
On 14 November 1942, Drew married Miss Sarah B. Kaylor in Pinellas County, Florida. They would have three daughters, Nancy, Bonnie and Jo Anne.
Colonel Drew was a combat pilot during World War II, the Korean War and the Vietnam War. He commanded the 309th Strategic Fighter Squadron from January to October 1955, flying the Republic F-84 Thunderjet. In August 1957, he became the first commanding officer of the 481st Fighter Bomber Squadron at Bergstom Air Force Base, Austin, Texas. Lieutenant Colonel Drew commanded the 354th Tactical Fighter Squadron at George Air Force Base, California, from 1962 to 1964, flying the Republic F-105D Thunderchief, and briefly commanded the 355th Tactical Fighter Wing.
Two weeks before a scheduled promotion to Brigadier General, Colonel Drew suffered a major heart attack and was forced to retire from the Air Force. He died 27 July 1985 at the age of 64 years. He was buried at Shawnee View Gardens Cemetery, Cumming, Georgia.
The McDonnell F-101 Voodoo was originally designed as a single-seat, twin-engine long range bomber escort, or “penetration fighter” for the Strategic Air Command, but was developed as a fighter bomber and reconnaissance airplane. The Voodoo first flew 29 September 1954, and the first F-101A was delivered to the Air Force 2 May 1957.
The F-101A was 67 feet, 5 inches (20.549 meters) long with a wingspan of 39 feet, 8 inches (12.090 meters). It was 18 feet (5.486 meters) high. The Voodoo weighed 24,970 pounds (11,245 kilograms) empty and had a maximum takeoff weight of 50,000 pounds (22,680 kilograms).
The standard F-101A was equipped with two Pratt and Whitney J57-P-13 afterburning turbojet engines. The J57 was a two-spool axial-flow turbojet which had a 16-stage compressor (9 low- and 7 high-pressure stages), 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, and 15,800 pounds (70.28 kilonewtons) with afterburner.
The J57-P-55 engines installed in the JF-101A were rated at 10,700 pounds of thrust (49.60 kilonewtons), and 16,900 pounds (75.18 kilonewtons) with afterburner. They were 20 feet, 11.93 inches (6.399 meters) long, 3 feet, 4.5 inches (1.029 meters) in diameter, and weighed 5,215 pounds (2,365 kilograms).
The maximum speed of the F-101A was 1,009 miles per hour (1,624 kilometers per hour) at 35,000 feet (10,668 meters). Its service ceiling was 55,800 feet (17,008 meters). It carried 2,341 gallons (8,862 liters) of fuel internally. With external tanks, the fighter bomber had a maximum range of 2,925 miles (4,707.3 kilometers).
The F-101A was armed with four 20mm Pontiac M39 single-barreled revolver cannon, with 200 rounds per gun. It could carry a Mark 28 bomb on a centerline mount.
McDonnell JF-101A Voodoo 53-2426 is on static display at Cannon Air Force Base, New Mexico.
A McDonnell Aircraft Corporation film about Operations Sun Run and Fire Wall is available of YouTube: