Tag Archives: Fighter

14 January 1950

This is the second Mikoyan Gurevich I 330 prototype, SI 02.
This is the second Mikoyan Gurevich I 330 prototype, SI 02.

14 January 1950: The Mikoyan Gurevich prototype fighter I 330 SI made its first flight with test pilot Ivan Ivashchenko. It would be developed into the MiG 17.

The MiG 17 was an improved version of the earlier MiG 15. It was a single-seat, single engine fighter armed with cannon, and capable of high subsonic and transonic speed.

Mikoyan Gurevich MiG 17.
Mikoyan Gurevich MiG 17.

The prototype’s wings were very thin and this allowed them to flex. The aircraft suffered from “aileron reversal,” in that the forces created by applying aileron to roll the aircraft about its longitudinal axis were sufficient to bend the wings and that caused the airplane to roll in the opposite direction.

The first prototype I 330 SI developed “flutter” while on a test flight, 17 March 1950. This was a common problem during the era, as designers and engineers learned how to build an airplane that could smoothly transition through the “sound barrier.” The rapidly changing aerodynamic forces caused the structure to fail and the horizontal tail surfaces were torn off. The prototype went into an unrecoverable spin. Test pilot Ivashchenko was killed.

Two more prototypes, SI 02 and SI 03, were built. The aircraft was approved for production in 1951.

More than 10,000 MiG 17 fighters were built in the Soviet Union, Poland and China. The type remains in service with North Korea.

A MiG 17 in flight.
A MiG 17 in flight.
Иван Т. Иващенко летчик-испытатель
Иван Т. Иващенко летчик-испытатель

Ива́н Тимофе́евич Ива́щенко (Ivan T. Ivashchenko) was born at Ust-Labinsk, Krasnodar Krai, Russia, 16 October 1905. He served in the Red Army from 1927 to 1930. He graduated from the Kuban State University in 1932.

Ivashchenko was trained as a pilot at the Lugansk Military Aviation School at Voroshilovgrad, and a year later graduated from the Kachin Military Aviation College at Volgograd.

In 1939, he fought in The Winter War. During the Great Patriotic War, Ivan Ivashchenko flew with a fighter squadron in the defense of Moscow.

From 1940 to 1945, Ivan Ivashchenko was a test pilot. He trained at the M.M. Gromov Flight Research Institute at Zhokovsky, southeast of Moscow, in 1941. He was assigned to Aircraft Factory No. 18 at Kuibyshev (Samara) from 1941 to 1943. Ivashchenko flew the Ilyushin Il-2 Sturmovik fighter bomber extensively. From 1943 to 1945 he was a test pilot for Lavochkin OKB at Factory 301 in Khimki, northwest of Moscow.

In 1945 Ivashchenko was reassigned to OKB Mikoyan, where he worked on the development of the MiG 15 and MiG 17 fighters. He participated in testing ejection seat systems and in supersonic flight.

Ivan T. Ivashchenko was a Hero of the Soviet Union, and was awarded the Order of Lenin, Order of the Red Banner (two awards) and Order of the Patriotic War. Killed in the MiG 17 crash at the age of 44 years, he was buried at the Novodevichy Cemetery in Moscow.

© 2017, Bryan R. Swopes

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13 January 2012

F-15E-47-MC Strike Eagle 89-0487 at Bagram Airfield, Afghanistan, 13 January 2012. (Photograph by Airman 1st Class Ericka Engblom, USAF)
McDonnell Douglas F-15E-47-MC Strike Eagle 89-0487, assigned to the 335th Expeditionary Fighter Squadron, taxis into its revetment at Bagram Airfield, Afghanistan, 13 January 2012. Note the World War II Eagle Squadron insignia and the green star kill mark painted on the fighter bomber’s nose. (Photograph by Airman 1st Class Ericka Engblom, USAF)

13 January 2012: This McDonnell Douglas F-15E-47-MC Strike Eagle, 89-0487, became the first F-15 to have logged over 10,000 flight hours. Regularly assigned to Captain Justin Pavoni, Pilot, and Lieutenant Colonel David Moeller, Weapons System Officer and commander of the 335th Expeditionary Fighter Squadron, on the mission which achieved the milestone, 487 was flown by Captain Ryan Bodenheimer, pilot, and Captain Erin Short, WSO, the two youngest flyers in the squadron.

89-0487 was accepted by the Air Force on 13 November 1990. At the time of this event, 487 was considered to be the flag ship of the 335th Expeditionary Fighter Squadron. During a three month period at Bagram Air Base, this individual F-15E flew 1,200 hours and dropped 15% of all the bombs dropped by the squadron.

During Operation Desert Storm, Captains Tim Bennett and Dan Bakke, USAF, flying this F-15E, call sign “Packard 41,” used a GBU-10 Paveway II 2,000-pound laser-guided bomb to “shoot down” an Iraqi Mi-24 Hind attack helicopter. 487 is the only F-15E to have scored an air-to-air victory.

This airplane is still in service with the United States Air Force. It passed 12,000 flight hours on 16 August 2016. It has been deployed for combat operations 17 times.

McDonnell Douglas F-15E Strike Eagle 89-0487 lands at Bagram Air Base after passing its 10,000th flight hour, 13 January 2012. (Airman 1st Class Ericka Engblom, U.S. Air Force)
With Captains Bodenheimer and Short in the cockpit, McDonnell Douglas F-15E-47-MC Strike Eagle 89-0487 lands at Bagram Airfield, Afghanistan, after passing its 10,000th flight hour, 13 January 2012. (Airman 1st Class Ericka Engblom, U.S. Air Force)

The Strike Eagle was begun as a private venture by McDonnell Douglas. Designed to be operated by a pilot and a weapons system officer (WSO), the airplane can carry bombs, missiles and guns for a ground attack role, while maintaining its capability as an air superiority fighter. It’s airframe was a strengthened and its service life doubled to 16,000 flight hours. The Strike Eagle became an Air Force project in March 1981, and  went into production as the F-15E. The first production model, 86-0183, made its first flight 11 December 1986.

The McDonnell Douglas F-15E Strike Eagle is a two-place twin-engine multi-role fighter. It is 63 feet, 9 inches (19.431 meters) long with a wingspan of 42 feet, 9¾ inches (13.049 meters) and height of 18 feet, 5½ inches (5.626 meters). It weighs 31,700 pounds (14,379 kilograms) empty and has a maximum takeoff weight of 81,000 pounds (36,741 kilograms). The F-15E is powered by two Pratt and Whitney F100-PW-229 turbofan engines which produce 17,800 pounds of thrust (79.178 kilonewtons) each, or 29,100 pounds (129.443 kilonewtons) with afterburner.

Captain Ryan Bodenheimer climbs down from the cockpit of F-15E Strike Eagle 89-0487 after completing the mission in which the aircraft passed the 10,000 flight hour mark. (U.S. Air Force)

The Strike Eagle has a maximum speed of Mach 2.54 (1,676 miles per hour, (2,697 kilometers per hour) at 40,000 feet (12,192 meters) and is capable of sustained speed at Mach 2.3 (1,520 miles per hour, 2,446 kilometers per hour). Its service ceiling is 60,000 feet (18,288 meters). The fighter-bomber has a combat radius of 790 miles (1,271 kilometers) and a maximum ferry range of 2,765 miles (4,450 kilometers).

Though optimized as a fighter-bomber, the F-15E Strike Eagle retains an air-to-air combat capability. The F-15E is armed with one 20mm M61A1 Vulcan 6-barrel rotary cannon with 512 rounds of ammunition, and can carry four AIM-9M Sidewinder heat-seeking missiles and four AIM-7M Sparrow radar-guided missiles, or a combination of Sidewinders, Sparrows and AIM-120 AMRAAM long range missiles. It can carry a maximum load of 24,500 pounds (11,113 kilograms) of bombs and missiles for ground attack.

This McDonnell Douglas F-15E Strike Eagle is carrying AIM-7 Sparrow and AIM-9 Sidewinder air-to-air missiles, 2,000-pound laser guided bombs, targeting designators and jettisonable fuel tanks. (U.S. Air Force)
This McDonnell Douglas F-15E Strike Eagle is carrying AIM-7 Sparrow and AIM-9 Sidewinder air-to-air missiles, 2,000-pound laser guided bombs, targeting designators and jettisonable fuel tanks. (U.S. Air Force)

© 2016, Bryan R. Swopes

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10 January 1956

Lieutenant Barty R. Brooks, USAFR, standing on the wing of a North American Aviation F-86F Sabre, Korea, 1954. (U.S. Air Force)

10 January 1956: First Lieutenant Barty Ray Brooks, United States Air Force Reserve, a pilot assigned to the 1708th Ferrying Wing, Detachment 12, at Kelly Air Force Base, Texas, along with two other pilots from the same unit, Captain Rusty Wilson and Lieutenant Crawford Shockley, picked up three brand new F-100C Super Sabre fighters at the North American Aviation Inc. assembly plant at Air Force Plant 42, Palmdale, California. It was to be a short flight, as these three jets were being taken to nearby George Air Force Base, Adelanto, California, only 42.5 miles (68.4 kilometers) to the east. Brooks was flying F-100C-20-NA, serial number 54-1907.

This North American Aviation F-100C-25-NA Super Sabre, serial number 54-2099, is similar to the fighter flown by Lieutenant Brooks, 10 January 1956. (U.S. Air Force)
This North American Aviation F-100C-25-NA Super Sabre, serial number 54-2099, is similar to the fighter flown by Lieutenant Brooks, 10 January 1956. (U.S. Air Force)
This photograph shows the lower section of the nose gear strut of an F-100 Super Sabre. The scissors ling is the hinged assembly. A red pin is visible at teh center hinge. Thi spin had been removed by ground handlers to tow the fighter, but had not been reinstalled before Lt. Brooks' flight.
This photograph shows the lower section of the nose gear strut of an F-100 Super Sabre. The scissors link is the hinged assembly. A red pin is visible at the center hinge. This pin had been removed by ground handlers to tow the fighter, but had not been secured with a safety pin when it was reinstalled before Lt. Brooks’ flight. (Michael Benolkin)

The brief flight was uneventful until the pilots lowered the landing gear to land at George AFB. One of the other pilots saw that the scissors link joining the upper and lower sections of the nose gear strut on Brooks’ Super Sabre was loose. Concerned that he would not be able to steer the fighter after touching down, Brooks diverted to Edward Air Force Base, 36 miles (57 kilometers) to the northwest, where a larger runway and more emergency equipment was available. Captain Wilson escorted Lieutenant Brooks to Edwards.

The F-100C Super Sabre had no flaps and required a high speed landing approach. Lieutenant Brooks had only 674 total flight hours as a pilot, and just 39 hours in the F-100.

During his final approach to the runway Brooks allowed the fighter to slow too much and the outer portion of the wings stalled and lost lift. This shifted the wings’ center of lift forward, which caused the airplane to pitch up, causing even more of the outer wing to stall.

Lieutenant Brooks fought to regain control of the airplane, but he was unable to. At 4:27 p.m., Pacific Standard Time, the F-100 crashed on the runway and exploded. Barty Ray Brooks was killed.

Edwards Air Force Base is the center of flight testing for the U.S. Air Force. In preparation for a test later that afternoon, the base film crews had their equipment set up along the runway and captured the last seconds of Brook’s flight on film. This is the most widely seen crash footage, and is still in use in pilot training. It is named “The Sabre Dance.”

Still image from cine film of Barty Brooks’ F-100C Super Sabre just before it crashed at Edwards Air Force Base, 10 January 1956. (U.S. Air Force)

Barty Ray Brooks was born in Martha Township,  Oklahoma, 2 December 1929. He was the third child of Benjamin Barto Brooks, a farmer, and Maye Henry Brooks. The family later moved to Lewisville, Texas. Brooks graduated from Lewisville High School in 1948, then studied agriculture at Texas A&M University, College Station, Texas.

Barty Ray Brooks, 1950. (Aggieland ’50)

While at Texas A&M, Brooks was a member of the Reserve Officers Training Corps (R.O.T.C.). On graduation, 30 May 1952, Brooks was commissioned as a second lieutenant, United States Air Force Reserve.

Lieutenant Brooks was trained as a pilot at Columbus Air Force Base, Mississippi, and Laredo Air Force Base, Texas. In 1954, he was assigned to the 311th Fighter Bomber Squadron, 58th Fighter Bomber Group, Taegu Air Base (K-2), Republic of South Korea. Brooks flew the Republic F-84 Thunderjet and North American Aviation F-86 Sabre. When he returned to the United States he was assigned to the 1708th Ferrying Wing.

The remains of 1st Lieutenant Barty Ray Brooks were interred at the Round Grove Cemetery, Lewisville, Texas.

The article, “The Deadly Sabre Dance,” by Alan Cockrell is highly recommended:

http://www.historynet.com/deadly-sabre-dance.htm

© 2018, Bryan R. Swopes

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8 January 1973

McDonnell F-4D-29-MC Phantom II 65-0796 at Yokota AB, Japan, 1972. (U.S. Air Force)
McDonnell F-4D-29-MC Phantom II 65-0796 at Yokota AB, Japan, 1972. (U.S. Air Force)

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.

Because of its advanced air search radars and digital computers, the nuclear-powered guided missile cruiser USS Long Beach (CGN-9) frequently served as RED CROWN. (U.S. Navy)

“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.”

"Craft 01", McDonnell F-4D-29-MC Phantom II 65-0796 on static display at William E. Dyess Elementary School, Abilene, Texas. (Abilene School District photo)
“Crafty 01”, McDonnell F-4D-29-MC Phantom II 65-0796 on static display at William E. Dyess Elementary School, Abilene, Texas. (Abilene School District photo)

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.

A Mikoyan Gurevich MiG-21 at the National Museum of the United States Air Force. (U.S. Air Force)
An Aero Vodochody-built MiG 21F-13 with the markings of the Vietnam Peoples’ Air Force at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force)

© 2017, Bryan R. Swopes

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8 January 1944

Lockheed XP-80 prototype, 44-83020, at Muroc AAF, 8 January 1944. (U.S. Air Force)
The Lockheed XP-80 prototype, 44-83020, at Muroc AAF, 8 January 1944. (Lockheed Martin Aeronautics Company)
Milo Burcham
Milo Garrett Burcham

8 January 1944: At Muroc Army Air Field (later to become Edwards Air Force Base), the Lockheed Aircraft Corporation’s chief engineering test pilot, Milo Garrett Burcham, took the prototype Model L-140, the Army Air Forces XP-80 Shooting Star, 44-83020, for its first flight.

Tex Johnston, who would later become Boeing’s Chief of Flight Test, was at Muroc testing the Bell Aircraft Corporation XP-59 Airacomet. He wrote about the XP-80’s first flight in his autobiography:

Early on the morning of the scheduled first flight of the XP-80, busload after busload of political dignitaries and almost every general in the Army Air Force arrived at the northwest end of the lake a short distance from our hangar. Scheduled takeoff time had passed. I was afraid Milo was having difficulties. Then I heard the H.1B fire up, and he taxied by on the lake bed in front of our ramp. What a beautiful bird—another product of Kelly Johnson, Lockheed’s famed chief design engineer—tricycle gear, very thin wings, and a clear-view bubble canopy. Milo gave me the okay sign.

This was the initial flight of America’s second jet fighter, and what a flight it was. Milo taxied along in front of generals and politicians, turned south and applied full power. I could see the spectators’ fingers going in their ears. The smoke and sand were flying as the engine reached full power, and the XP-80 roared down the lake. Milo pulled her off, retracted gear and flaps, and held her on the deck. Accelerating, he pulled up in a climbing right turn, rolled into a left turn to a north heading, and from an altitude I estimated to be 4,000 feet [1,219 meters] entered a full-bore dive headed for the buses. He started the pull-up in front of our hangar and was in a 60-degree climb when he passed over the buses doing consecutive aileron rolls at 360 degrees per second up to 10,000 feet [3,048 meters]. He then rolled over and came screaming back. He shot the place up north and south, east and west, landed and coasted up in front of the spectators, engine off and winding down. I have never seen a crowd so excited since my barnstorming days. I returned to the office and dictated a wire to [Robert M.] Stanley [Chief Test Pilot, Bell Aircraft Corporation] “WITNESSED LOCKHEED XP-80 INITIAL FLIGHT STOP VERY IMPRESSIVE STOP BACK TO DRAWING BOARD STOP SIGNED, TEX” I knew he would understand.

Tex Johnston: Jet-Age Test Pilot, by A.M. “Tex” Johnston with Charles Barton, Smithsonian Books, Washington, D.C., 1 June 1992, Chapter 5 at Pages 127–128.

A few minor problems caused Burcham to end the flight after approximately five minutes but these were quickly resolved and flight testing continued.

The XP-80 was the first American airplane to exceed 500 miles per hour (805 kilometers per hour) in level flight.

Clarence L. "Kelly" Johnson with a scale model of a Lockheed P-80A-1-LO Shooting Star. Johnson's "Skunk Works" also designed the F-104 Starfighter, U-2, A-12 Oxcart and SR-71A Blackbird. (Lockheed Martin Aeronautical Company)
Clarence L. “Kelly” Johnson with a scale model of a Lockheed P-80A-1-LO Shooting Star. Johnson’s “Skunk Works” also designed the F-104 Starfighter, U-2, A-12 Oxcart and SR-71A Blackbird. (Lockheed Martin Aeronautics Company)

The Lockheed XP-80 was designed by Clarence L. “Kelly” Johnson and a small team of engineers that would become known as the “Skunk Works,” in response to a U.S. Army Air Corps proposal to build a single-engine fighter around the de Havilland Halford H.1B Goblin turbojet engine. (The Goblin powered the de Havilland DH.100 Vampire F.1 fighter.)

Lockheed Aircraft Corporation was given a development contract which required that a prototype be ready to fly within just 180 days.

Milo Burcham, on the left, shakes hands with Clarence L. Johnson following the first flight of the Lockheed XP-80, 8 January 1944. (Lockheed)
Milo Burcham, on the left, shakes hands with Clarence L. Johnson following the first flight of the Lockheed XP-80, 8 January 1944. (Lockheed Martin Aeronautics Co.)

The XP-80 was a single-seat, single-engine airplane with straight wings and retractable tricycle landing gear. Intakes for engine air were placed low on the fuselage, just forward of the wings. The engine exhaust was ducted straight out through the tail. For the first prototype, the cockpit was not pressurized but would be on production airplanes.

As was customary for World War II U.S. Army Air Forces aircraft, the prototype was camouflaged in non-reflective Dark Green with Light Gull Gray undersides. The blue and white “star and bar” national insignia was painted on the aft fuselage, and Lockheed’s winged-star corporate logo was on the nose and vertical fin. Later, the airplane’s radio call, 483020 was stenciled on the fin in yellow paint. The number 20 was painted on either side of the nose in large block letters. Eventually the tip of the nose was painted white and a large number 78 was painted just ahead of the intakes in yellow block numerals. Early in the test program, rounded tips were installed on the wings and tail surfaces. This is how the XP-80 appears today.

Lockheed XP-80 parked at Muroc Dry Lake, 1944 (Lockheed)
The highly-polished Dark Green and Light Gull Gray Lockheed XP-80 prototype parked at Muroc Dry Lake, 1944 (Lockheed Martin Aeronautics Co.)

The XP-80 is 32 feet, 911/16 inches (9.9997 meters) long with a wingspan of 37 feet, ⅞-inch (11.2998 meters) and overall height of 10 feet, 21/16 inches (3.1004 meters). It had a Basic Weight for Flight Test of 6,418.5 pounds (2,911.4 kilograms) and Gross Weight (as actually weighed prior to test flight) of 8,859.5 pounds (4,018.6 kilograms).

The Halford H.1B Goblin used a single-stage centrifugal-flow compressor, sixteen combustion chambers, and single-stage axial-flow turbine. It had a straight-through configuration rather than the reverse-flow of the Whittle turbojet from which it was derived. The H.1B produced 2,460 pounds of thrust (10.94 kilonewtons) at 9,500 r.p.m., and 3,000 pounds (13.34 kilonewtons) at 10,500 r.p.m. The Goblin weighed approximately 1,300 pounds (590 kilograms).

Cutaway illustration of the Halford H.1B Goblin turbojet engine. (FLIGHT and AIRCRAFT ENGINEER)

The XP-80 has a maximum speed of 502 miles per hour (808 kilometers per hour) at 20,480 feet (6,242 meters) and a rate of climb of 3,000 feet per minute (15.24 meters per second). The service ceiling is 41,000 feet (12,497 meters).

Unusual for a prototype, the XP-80 was armed. Six air-cooled Browning AN-M2 .50-caliber machine guns were placed in the nose. The maximum ammunition capacity for the prototype was 200 rounds per gun.

The Halford engine was unreliable and Lockheed recommended redesigning the the fighter around the larger, more powerful General Electric I-40 (produced by GE and Allison as the J33 turbojet). The proposal was accepted and following prototypes were built as the XP-80A.

Lockheed built 1,715 P-80s for the U.S. Air Force and U.S. Navy. They entered combat during the Korean War in 1950. A two-seat trainer version was even more numerous: the famous T-33A Shooting Star.

Lockheed XP-80 Shooting Star 44-83020 was used as a test aircraft and jet trainer for several years. In 1949, it was donated to the Smithsonian Institution. 44-83020 is on display at the Jet Aviation exhibit of the National Air and Space Museum. It was restored beginning in 1976, and over the next two years nearly 5,000 man-hours of work were needed to complete the restoration.

The prototype Lockheed XP-80 Shooting Star, 44-83020, at teh Smithsonian Institution National Air and Space Museum. (NASM)
The prototype Lockheed XP-80 Shooting Star, s/n 140-1001, 44-83020, at the Smithsonian Institution National Air and Space Museum. (NASM)

© 2019, Bryan R. Swopes

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