20 April 1962: “Neil’s Cross-Country.” NASA Research Test Pilot Neil Alden Armstrong conducts a flight to test the Minneapolis-Honeywell MH-96 flight control system installed in the third North American Aviation X-15, serial number 56-6672. The new system combined both aerodynamic and reaction thruster flight controls in one hand controller rather than the two used in X-15s -670 and -671, simplifying the tasks for the pilot.
North American Aviation X-15A-3 56-6672 over Delamar Dry Lake, Nevada. (U.S. Air Force 161111-F-ZZ999-001)
On its fourth flight, -672 was air-dropped from the Boeing NB-52B Stratofortress drop ship, Balls 8, over Mud Lake, Nevada. Armstrong fired the Reaction Motors XLR99-RM-1 engine and let it burn for 82.4 seconds. The X-15 accelerated to Mach 5.31 (3,789 miles per hour/6,098 kilometers per hour). After the engine was shut down, the rocketplane continued to its peak altitude on a ballistic trajectory, reaching 207,500 feet (63,246 meters) before going over the top and beginning its descent back toward the atmosphere. The test of the new flight control system went well.
Neil Armstrong began to pull out of the descent at about 100,000 feet (30,480 meters), but the X-15 “ricocheted” off the top of the atmosphere and climbed back to 115,000 feet (35,052 meters) where the aerodynamic control surfaces could not function. He used the reaction thrusters to turn toward the dry lake landing area at Edwards Air Force Base, but although the X-15 rolled into a left bank, it would not change direction and still in ballistic flight, went zooming by Edwards at Mach 3 and 100,000 feet in a 90° left bank.
Rogers Dry Lake and Edwards Air Force Base are at the top of this image, right of center. The Rose Bowl is marked near the bottom, left of center. (Google Maps)
As the X-15 dropped back into the atmosphere, Armstrong was finally able to get it slowed down, but he was far south of his planned landing site. By the time he got -672 turned around he was 45 miles (72.4 kilometers) to the south, over the Rose Bowl in Pasadena, and gliding through 45,000 feet (13,716 meters). There was real doubt that he would be able to make the X-15 stretch its glide to reach the dry lake.
In a masterful display of airmanship, Neil Armstrong was able to get the X-15 to reach the south end of the dry lake, 12 miles (19.3 kilometers) from the planned landing spot to the north. But it was a very close call. In debriefing, the pilots of the four F-104 chase planes were asked how much clearance Armstrong had as he crossed over the Joshua trees at the edge of the lake bed. One of them answered, “Oh, at least 100 feet—on either side.”
At 12 minutes, 28.7 seconds, this was the longest flight of the entire X-15 program. It is called “Neil’s cross-country flight.”
A U.S. Navy fighter pilot who flew 78 combat missions during the Korean War, Neil Armstrong became a civilian test pilot at NACA (National Advisory Committee on Aeronautics, the predecessor to NASA) in 1955. He made 7 flights in the X-15 before transferring to NASA’s Project Gemini in 1962.
Armstrong was command pilot for Gemini 8 and Gemini 11, commander of the backup flight crew of the Apollo 8 mission, and was commander of Apollo 11.
On 20 July 1969, Neil Alden Armstrong was the First Man To Stand on the Surface of The Moon.
Squadron Leader Marmaduke Thomas St. John “Pat” Pattle, Officer Commanding No. 33 Squadron, Royal Air Force, and the Squadron Adjutant, Flight Lieutenant George Rumsey, standing by a Hawker Hurricane at Larissa, Thessaly, Greece, March–April 1941. (IWM)
20 April 1941: Squadron Leader Marmaduke Thomas St. John Pattle, D.F.C. and Bar, Royal Air Force, commanding No. 33 Squadron, was killed in action during the Battle of Athens when his Hawker Hurricane fighter was shot down by two or more Luftwaffe Messerschmitt Bf 110 fighters. Pattle’s airplane crashed into the sea near the Port of Piraeus, southwest of Athens.
Messerschmitt Bf 110 twin-engine heavy fighter, circa 1942. (Deutsches Bundesarchiv)
Squadron Leader Pattle may have been the highest-scoring Allied fighter ace of World War II. The exact number of enemy aircraft destroyed cannot be determined precisely because records were lost or destroyed during the Battle of Greece. The last officially acknowledged score was 23 airplanes shot down, mentioned in The London Gazette with the notice of the award of a Bar to his Distinguished Flying Cross. It is widely acknowledged that he shot down many more, and on at least two occasions, shot down five enemy airplanes in one day. Authors who have researched Pattle’s combat record believe that he shot down at least 50, and possibly as many as 60 aircraft.
For comparison, Air Vice Marshal James Edgar (“Johnnie”) Johnson, C.B., C.B.E., D.S.O. and Two Bars, D.F.C. and Bar, is officially credited by the Royal Air Force with shooting down 34 enemy airplanes. Colonel Francis Stanley (“Gabby”) Gabreski, United States Air Force, was credited with 28 kills during World War II. In the Pacific Theater of Operations, Major Richard Ira Bong is officially credited with 40 enemy airplanes shot down.
Marmaduke Thomas St. John Pattle was born at Butterworth, Cape Province, South Africa, 23 July 1914. He was the son of Sergeant-Major William John Pattle, British Army, and Edith Brailsford Pattle. After failing to be accepted by the South African Air Force, at the age of 21 years, he traveled to Britain to apply to the Royal Air Force. He was offered a short-service commission and sent to flight school.
Pattle was commissioned as an Acting Pilot Officer on probation, effective 24 August 1936. He trained as a fighter pilot in the Gloster Gauntlet, and was rated as exceptional. He was then assigned to No. 80 Squadron, which was equipped with the newer Gloster Gladiator. He was confirmed in the rank of Pilot Officer 29 June 1937.
Prototype Gloster Gladiator in flight, now marked K5200.
No. 80 Squadron was sent to Egypt to protect the Suez Canal. With the United Kingdom’s declaration of war on the Axis powers, Pattle and his unit were soon in combat with the Regia Aeronautica (the Italian Royal Air Force) across North Africa. He shot down his first enemy airplanes, a Breda Ba.65 and a Fiat CR.42, on 4 August 1940. Unfortunaely, Pattle was also shot down and he had to walk across the Libyan desert to friendly lines.
Distinguished Flying Cross
Pattle was promoted to Flight Lieutenant, 3 September 1940. He is credited with having shot down at least 15 Italian airplanes with the Gladiator.
In February 1941, No. 80 Squadron began flying the Hawker Hurricane. This was a huge technological advance over the Gladiator, and the Hurricane’s eight .303-caliber machine guns doubled the firepower of the biplane. The squadron was sent to Greece, where it would engage the Luftwaffe.
Flight Lieutenant Pattle was awarded the Distinguished Flying Cross, 11 February 1941. The following month, 12 March 1941, Pat Pattle was promoted to Acting Squadron Leader, and given command of No. 33 Squadron at Larissa, Thessaly, Greece.
Squadron Leader Pattle was awarded a Bar to his DFC (a second award), 18 March 1941.
Pilots of No. 33 Squadron, Royal Air Force, with a Hawker Hurricane Mk.I fighter, V7419. Pattle is in the first row, seated, fifth from left. (Imperial War Museum)
Designed by Sydney Camm to meet a Royal Air Force Specification for a high speed monoplane interceptor, the airplane was designed around the Rolls-Royce PV-12 engine. The prototype Hawker Hurricane, K5083, first flew 6 November 1935.
The Hurricane was built in the traditional means of a light but strong framework covered by doped linen fabric. Rather than wood, however, the Hurricane’s framework used high strength steel tubing for the aft fuselage. A girder structure covered in sheet metal made up the forward fuselage. A primary consideration of the fighter’s designer was to provide good visibility for the pilot.
The Hawker Hurricane Mk.I was ordered into production in the summer of 1936. The first production airplane flew on 12 October 1937. The Hurricane Mk. I was 31 feet, 5 inches (9.576 meters) long with a wingspan of 40 feet, 0 inches (12.192 meters), and overall height of 10 feet, 6 inches (3.200 meters). Its empty weight was 5,234 pounds (2,374 kilograms) and maximum gross weight was 6,793 pounds (3,081 kilograms).
The Mk.I’s engine was a liquid-cooled, supercharged, 27.01 liter (1,648.96 cubic inches) Rolls-Royce R.M.1.S. Merlin Mk.III single-overhead-cam 60° V-12, rated at 990 horsepower at 2,600 r.p.m. at 12,250 feet (3,734 meters), and 1,030 horsepower at 3,000 r.p.m., at 10,250 feet (3,124 meters), using 87 octane aviation gasoline. The Merlin III drove the propeller through a 0.477:1 gear reduction ratio. It weighed 1,375 pounds (624 kilograms).
The fixed-pitch propeller was soon replaced with a three-bladed, two-pitch propeller, and then a three-bladed constant-speed propeller. Speed trials of a Mk.I equipped with a 10 foot, 9 inch (3.277 meters) diameter Rotol constant-speed propeller achieved a maximum True Air Speed in level flight of 316 miles per hour (509 kilometers per hour) at 17,500 feet (5,334 meters). The service ceiling was 32,250 feet (9,830 meters). The Mk.I’s range was 600 miles (966 kilometers) at 175 miles per hour (282 kilometers per hour).
The Hurricane Mk.I could climb to 20,000 feet in 9.7 minutes.
The fighter was armed with eight Browning .303 Mark II machine guns mounted in the wings, with 334 rounds of ammunition per gun.
Hawker Hurricane Mk.I at NACA Langley Memorial Aeronautical Laboratory. (NASA)
Howard Picton flies the Sopwith Tabloid float plane during the 1914 Schneider Trophy Race at Monaco.
20 April 1914: Cecil Howard Pixton, flying a Sopwith Tabloid float plane, wins the Coupe d’Aviation Maritime Jacques Schneider (commonly called the Schneider Trophy). Pixton completed 28 laps of a 10-kilometer triangular course at Monaco in 2 hours, 13-2/5 seconds. His average speed for the race was 137.442 kilometers per hour (85.403 miles per hour).
Schneider Trophy Race Course, Monaco, 20 April 1914.
Pixton flew two additional laps, a total of 300 kilometers, in 2 hours, 9 minutes, 10 seconds, for an overall average speed of 139.355 kilometers per hour (86.591 miles per hour).
Mechanic Victor Mahl, Cecil Howard Pixton, and Thomas Octave Murdoch Sopwith with a wheel-equipped Sopwith Tabloid.
The Sopwith Tabloid was designed by Harry George Hawker. It was a single-place, single-engine, single-bay biplane. The prototype was equipped with skid landing gear, but this was soon changed to wheels. Roll control was accomplished by wing-warping. The single Schneider Cup racer had two floats under the wings and a small float under the tail. The racer was equipped with a 100-horsepower Gnome Monosoupape engine, turning a two-blade fixed-pitch propeller.
The Schneider Cup-winning Sopwith Tabloid.The Schneider Cup-winning Sopwith Tabloid.
Albert Scott Crossfield, Jr., with the Victor Black Edition Continental IO-470-E engine installed in his Cessna 210A, N6579X. The engine was overhauled by Victor Aviation of Palo Alto, California. (Victor Aviation)
19 April 2006: Former experimental test pilot Albert Scott Crossfield, Jr., was enroute from Prattville, Alabama, to Manassas, Virginia. Crossfield was flying his personal Cessna 210A, N6579X. The Cessna was cruising at 11,000 feet (3,353 meters) under Instrument Flight Rules (IFR), and under the control of the Atlanta Air Route Traffic Control Center (ARTCC).
During the flight, he encountered a Level 6 thunderstorm.
Crossfield requested to deviate from his planned course to avoid the severe turbulence. Atlanta Center authorized his request and he began to turn. Approximately 30 seconds later, at 11:10 a.m., radar contact was lost near Ludville, Georgia. The last indication was that the Cessna was descending through 5,500 feet (1,676 meters).
The wreckage of N6579X was located the following day by a Civil Air Patrol search team, 3.3 nautical miles (6.1 kilometers) northwest of Ludville at an elevation of 1,269 feet (386.8 meters) above Sea Level. [N. 34° 30.767′, W. 84° 39.492′] The airplane had descended through the forest canopy nearly vertically and created a crater approximately 4½ feet (1.4 meters) deep and 6 feet (1.8 meters) across. Albert Scott Crossfield’s body was inside.
Scott Crossfield’s 1962 Cessna 210A Centurion, photographed at Santa Monica Airport, California, 26 September 1999. (AirNikon Collection, Pima Air & Space Museum, Tucson, Arizona, via airliners.net. Image used with permission.)
N6579X was a Cessna Model 210A, serial number 21057579, built in 1960 by the Cessna Aircraft Company, Inc., of Wichita Kansas. It was a six-place, single-engine, high-wing monoplane with external struts to brace the wings, and retractable, tricycle landing gear. The airplane was certified for instrument flight by a single pilot. At the time of the crash, N6579X had been flown 4,987.4 hours, total time since new (TTSN).
The Cessna 210A was 28 feet, 2 inches (8.585 meters) long with a wingspan of 36 feet, 6 inches (11.125 meters) and overall height of 9 feet, 7 inches (2.921 meters). The airplane had an empty weight of 1,839 pounds (834.2 kilograms) and maximum gross weight of 2,900 pounds (1,315.4 kilograms). It had a fuel capacity of 65 gallons (246 liters), with 10 gallons (37.9 liters) unusable, and 12 quarts of engine oil (11.4 liters).
N6579X was powered by an air-cooled, fuel-injected, 471.239-cubic-inch-displacement (7.722 liters) Teledyne Continental IO-470-E horizontally-opposed six-cylinder direct-drive engine with a compression ratio of 8.6:1. The engine was rated at 260 horsepower at 2,625 r.p.m. for takeoff, using 100LL aviation gasoline. It weighed 429 pounds (195 kilograms). This engine, serial number 77583-0-E, was original to the airplane and accumulated 4,987.4 hours, total time since new (TTSN). It had been overhauled by Victor Aviation, Palo Alto, California, 1,259.8 hours prior to the accident (TSO). A three-bladed McCauley constant-speed propeller with a diameter of 6 feet, 10 inches (2.083 meters) was installed in 2005.
The Cessna Model 210A has a maximum structural cruise speed (VNO) of 175 miles per hour (282 kilometers), and maximum speed (VNE) of 200 miles per hour (322 kilometers per hour). Maneuvering speed, which should be used in turbulent conditions, is 130 miles per hour (209 kilometers per hour). The 210A has a maximum rate of climb of 1,300 feet per minutes (6.6 meters per second) and service ceiling of 20,700 feet (6,309 meters). Its maximum range is 1,284 miles (2,066 kilometers).
Albert Scott Crossfield, Jr., aeronautical engineer and test pilot, 1921-2006. (Jet Pilot Overseas)
Albert Scott Crossfield, Jr., was born 2 October 1921 at Berkeley, California. He was the second of three children of Albert Scott Crossfield, a chemist who was employed as the superintendant of the Union Oil Company refinery in Wilmington, California, and Lucia M. Dwyer Crossfield.
When he was five years old, young “Scotty” contracted pneumonia. He was comatose for a while and was not expected to survive, but after several weeks he began to recover. A year later, he again became seriously ill, this time with rheumatic fever. He was confined to total bed rest for four months, and continued to require extensive bed rest until he was about ten years old. It was during this time that he became interested in aviation.
Scott Crossfield attended Boistfort Consolidated School, southwest of Chehalis, Washington, graduating in 1939, and then studied engineering at the University of Washington until taking a job at Boeing in late 1941. During this time, Scotty learned to fly in the Civilian Aviation Training Program.
The week following the attack on Pearl Harbor and the United States’ entry into World War II, Scott Crossfield enlisted as an aviation cadet in the United States Army Air Corps. After numerous delays, he joined the United States Navy on 21 February 1942, and resigned from the Air Corps. He began aviation cadet training at NAS Sand Point, near Seattle, and then was sent to NAS Corpus Christi, Texas. In December 1942, he graduated, received his gold Naval Aviator wings and was commissioned as an Ensign, United States Naval Reserve.
Ensign Crossfield was assigned to NAS Kingsville, near Kingsville, Texas, as an advanced bombing and gunnery instructor.
In April 1943 at Corpus Christi, Texas, Ensign A. Scott Crossfield married Miss Alice Virginia Knoph of Seattle. They would have nine children.
Ensign Crossfield served as a gunnery instructor for two years. He was promoted to Lieutenant (junior grade), 1 March 1944. In 1945 he was transferred to Air Group 51 in the Hawaiian Islands, which was preparing for the invasion of Japan. Crossfield was promoted to Lieutenant, 1 August 1945, while serving aboard the Independence-class light aircraft carrier USS Langley (CVL-27). With the end of World War II, though, the Navy was cutting back. Lieutenant Crossfield was released from active duty 31 December 1945.
Following the War, Scotty returned to the University of Washington to complete his degree. He took a part time job operating the University’s wind tunnel. At the same time, he remained in the Naval Reserve, assigned to VF-74, a fighter squadron which flew both the Grumman F6F Hellcat and Chance Vought F4U Corsair out of NAS Sand Point, back where his naval career began.
Chance Vought F4U-4 Corsair, Bu. No. 82034, assigned to Fighter Squadron 74 (VF-74). (United States Navy)
Crossfield graduated from the University of Washington with a bachelor’s degree in aeronautical engineering in June 1949, and a master’s degree in 1950.
In 1950 Crossfield joined the National Advisory Committee for Aeronautics (NACA) as a research test pilot at the High-Speed Flight Station, Edwards Air Force Base, California. He flew the Republic YF-84, F-84F Thunderstreak, and North American Aviation F-86 Sabre. Crossfield made 25 flights in the delta-winged Convair XF-92A, which he described as “the worst flying airplane built in modern times.” He also flew the Northrop X-4 and Bell X-5. He made 17 flights conducting stability tests in the Douglas D-558-1 Skystreak. Scotty made 65 flights in the North American Aviation F-100A Super Sabre, including a test series which discovered a fatal flaw which led to the death of North American’s chief test pilot, George S. Welch.
NACA Research Test Pilot Albert Scott Crossfield in the cockpit of the Douglas D-558-II Skyrocket after exceeding Mach 2, 20 November 1953. (NASA)
Crossfield is known as a rocketplane pilot. He made 10 flights in the Bell X-1, 89 in the Douglas D-558-II Skyrocket, and 14 in the North American Aviation X-15. He became the first pilot to exceed Mach 2 when he flew the Skyrocket to Mach 2.005, 20 November 1953.
Scott Crossfield discusses the X-15 with North American Aviation engineers Edmond R. Cokeley and Charles H. Feltz. (North American Aviation, Inc.)
Crossfield flew for NACA for approximately five years. During that time, approximately 500 flights were made at Edwards by NACA test pilots. Scott Crossfield flew 181 of them.
Scott Crossfield left NACA in 1956 to join North American Aviation, Inc., as chief engineering test pilot for the X-15 project. Between 8 June 1959 and 6 December 1960, he made fourteen flights in the X-15. He reached a maximum speed of Mach 2.97 and altitude of 88,116 feet (26,858 meters). Once the contractor’s flight tests were completed and the rocketplane turned over to the U.S. Air Force and NACA, the customers’ test pilots, Joe Walker and Major Robert M. White, took over.
Albert Scott Crossfield made 113 flights in rocket-powered aircraft, more than any other pilot.
After completing his work on the X-15, Crossfield followed Harrison (“Stormy”) Storms, who had been the Chief Engineer of North American’s Los Angeles Division (where the X-15 was built) to the Space and Information Systems Division in Downey, California, where he worked in quality assurance, reliability engineering and systems testing for the Apollo Command and Service Modules and the Saturn S-II second stage.
Crossfield left North American at the end of 1966, becoming Vice President for Technological Development for Eastern Air Lines. In this position, he flew acceptance tests for new Boeing 720 and 727 airliners at Boeing in Seattle.
In The X-15 Rocket Plane, author Michelle Evans quoted Crossfield as to why he had not entered NASA’s space program as an astronaut:
One question that pressed was, with his love of flight and the early responsibility of going into space with the X-15, why would Scott not apply to the NASA astronaut office? He explained, “[Dr.] Randy Lovelace and General [Donald] Flickinger were on the selection board. They took me to supper one night and asked me not to put in for astronaut. I asked them, ‘Why not?’ and they said, ‘Well, we’re friends of yours. We don’t want to have to turn you down.’ I asked, ‘Why would you have to turn me down?’ and they said, ‘You’re too independent.’ “
—The X-15 Rocket Plane: Flying the First Wings into Space, by Michelle, Evans, University of Nebraska Press, 2013, Chapter 1 at Page 33.
The remains of Albert Scott Crossfield are interred at the Arlington National Cemetery.
Scott Crossfield is in the cockpit of X-15 56-6670, under the right wing of NB-52A 52-003. (NASA)
Lieutenant Colonel Leo Keith Thorsness, United States Air Force. (U.S. Air Force)
MEDAL OF HONOR
LIEUTENANT COLONEL LEO K. THORSNESS UNITED STATES AIR FORCE
Rank and organization: Lieutenant Colonel (then Major), U.S. Air Force, 357th Tactical Fighter Squadron
Place and date: Over North Vietnam, 19 April 1967.
Entered service at: Walnut Grove, Minn.
Born: 14 February 1932, Walnut Grove, Minn.
Citation: For conspicuous gallantry and intrepidity in action at the risk of his life above and beyond the call of duty. As pilot of an F- 105 aircraft, Lt. Col. Thorsness was on a surface-to-air missile suppression mission over North Vietnam. Lt. Col. Thorsness and his wingman attacked and silenced a surface-to-air missile site with air-to-ground missiles, and then destroyed a second surface-to-air missile site with bombs. In the attack on the second missile site, Lt. Col. Thorsness’ wingman was shot down by intensive antiaircraft fire, and the 2 crewmembers abandoned their aircraft. Lt. Col. Thorsness circled the descending parachutes to keep the crewmembers in sight and relay their position to the Search and Rescue Center. During this maneuver, a MIG-17 was sighted in the area. Lt. Col. Thorsness immediately initiated an attack and destroyed the MIG. Because his aircraft was low on fuel, he was forced to depart the area in search of a tanker. Upon being advised that 2 helicopters were orbiting over the downed crew’s position and that there were hostile MiGs in the area posing a serious threat to the helicopters, Lt. Col. Thorsness, despite his low fuel condition, decided to return alone through a hostile environment of surface-to-air missile and antiaircraft defenses to the downed crew’s position. As he approached the area, he spotted 4 MIG-17 aircraft and immediately initiated an attack on the MlGs, damaging 1 and driving the others away from the rescue scene. When it became apparent that an aircraft in the area was critically low on fuel and the crew would have to abandon the aircraft unless they could reach a tanker, Lt. Col. Thorsness, although critically short on fuel himself, helped to avert further possible loss of life and a friendly aircraft by recovering at a forward operating base, thus allowing the aircraft in emergency fuel condition to refuel safely. Lt. Col. Thorsness’ extraordinary heroism, self-sacrifice, and personal bravery involving conspicuous risk of life were in the highest traditions of the military service, and have reflected great credit upon himself and the U.S. Air Force.
Major Leo K. Thorsness and Captain Harold E. Johnson with their Republic F-105F Thunderchief, Takhli Royal Thai Air Force Base, Thailand, 1967. (U.S. Air Force)
AIR FORCE CROSS
CAPTAIN HAROLD EUGENE JOHNSON
Air Force Cross
The President of the United States of America, authorized by Title 10, Section 8742, United States Code, takes pleasure in presenting the Air Force Cross to Captain Harold Eugene Johnson (AFSN: 0-3116556/42372A), United States Air Force, for extraordinary heroism as Electronics Warfare Officer of an F-105 aircraft of the 357th Tactical Fighter Squadron, 355th Tactical Fighter Wing, Tuy Hoa Air Base, Vietnam, engaged in a pre-strike, missile suppression mission over North Vietnam on 19 April 1967. On that date, Captain Johnson guided his pilot in attacking and destroying a surface-to-air missile installation with an air-to-ground missile. Through his technical skill, he immediately detected a second missile complex and guided the pilot into visual contact. Diving into a deadly barrage of anti-aircraft fire, his aircraft bombed and successfully destroyed this site. In the attack on this second missile site, a wingman was shot down by the intense anti-aircraft fire, and the crew members were forced to abandon their aircraft. Flying through hostile missile threats, Captain Johnson’s aircraft engaged and destroyed a MiG-17 while attacking a superior MiG force. He aided in the rescue efforts for the downed crew, engaged additional MiGs, and damaged one in the encounter. Through his extraordinary heroism, superb airmanship, and aggressiveness, Captain Johnson has reflected the highest credit upon himself and the United States Air Force.
General Orders: Department of the Air Force, Special Order GB-363 (April 19, 1967)
Action Date: 19-Apr-67
Service: Air Force
Rank: Captain
Company: 357th Tactical Fighter Squadron
Regiment: 355th Tactical Fighter Wing
Division: Tuy Hoa Air Base, Vietnam
Major Thorsness and Captain Johnson flew this Republic F-105F-1-RE Thunderchief, 63-8301, on 19 April 1967. It was one of 61 F-105Fs that were upgraded to the F-105G Wild Weasel III configuration beginning in late 1967. It survived the Vietnam War, but was destroyed 20 December 1974 when, assigned to the 35th TFW at George AFB, California, it crashed at the Cuddeback Lake Gunnery Range after an engine failure. (U.S. Air Force)
A description of the air battle follows:
The first MiG kill of the day was recorded by Maj. Leo K. Thorsness, pilot, and Capt. Harold E. Johnson, Electronic Warfare officer (EWO), flying an F-105F. Thorsness’ flight consisted of four F-105F Wild Weasel aircraft, each plane being manned by a pilot and EWO and being specially equipped to locate and attack SAM sites. The flight was ahead of the main strike force and was committed to suppress SAM activity in the target area. About 8 to 10 MiG-17s attacked as the flight prepared to strike a SAM radar site with Shrike air-to-ground missiles. The Thorsness flight split up into three parts: the third and fourth aircraft entered into separate MiG engagements while Thorsness and his wingman continued the attack against the radar. The time was then about 4:55 p.m. Johnson provides an account of the encounter:
We found and delivered our ordnance on an occupied SAM site. As we pulled off the site heading west, Kingfish 02 ¹ called that he had an overheat light. He also headed west, and the crew, Majors Thomas M. Madison, pilot, and Thomas J. Sterling, EWO, had to eject from their aircraft. We headed toward them by following the UHF-DF steer we received from their electronic beepers and saw them in the chutes. . .
As we circled the descending crew, we were on a southerly heading when I spotted a MiG-17 heading east, low at out 9 o’clock position. I called him to the attention of Major Thorsness. . . .
Thorsness continued the story:
The MiG was heading east and was approximately 2,500 feet mean sea level. We were heading southeast and at 8,000 feet MSL. I began “S” turning to get behind the MiG. After one and a half “S” turns the MiG had progressed from the foothills over the delta southwest of Hanoi. The MiG turned to a northerly heading, maintaining approximately the same altitude and airspeed. Captain Johnson continued to give me SAM bearings, SAM-PRF [pulse recurrence frequency] status and launch indications as I continued to maneuver to attain a 6 o’clock position on the MiG.
The first burst of approximately 300 rounds of 20 mm was fired from an estimated 2,000–1,500 feet in a right hand shallow pursuit curve, firing with a cased sight reticle. No impacts were observed on the MiG. Within a few seconds we were in the 6 o’clock position with approximately 75 to 100 knots overtake speed. I fired another burst of approximately 300 rounds of 20 mm. I pulled up to avoid both the debris and the MiG. While pulling up I rolled slightly to the right, then left. The MiG was approximately 100 feet low and to our left, rolling to the right. The two red stars were clearly discernible, one on top of each wing, and several rips were noted on the battered left wing. We continued to turn to the left and after turning approximately 130° again sighted the MiG, still in a right descending spiral. Just prior to the MiG’s impacting the ground, Captain Johnson sighted a MiG-17 at our 6:30 position approximately 2,000 feet back. I pulled into a tighter left turn, selected afterburner, and lowered the nose. I again looked at the crippled MiG, saw it impact the ground in what appeared to be a rice field. After confirming the MiG had in fact impacted the ground I made a hard reversal and descended very near the ground, heading generally westerly into the foothills.
Thorsness then left the battle area, but returned after refueling to provide rescue combat air patrol during the search for his wingman’s aircrew. Thorsness and Johnson attacked another MiG and scored some damaging hits before they were themselves attacked by other MiG-17s. Although it is highly probable that Thorsness and Johnson destroyed a second MiG, this kill was not confirmed.
— 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 Pages 46 and 47.
Eleven days later, 30 April 1967, Major Thorsness and Captain Johnson were shot down by an AA-2A Atoll heat-seeking missile fired by a MiG-21 fighter piloted by Vũ Ngọc Đỉnh, 921st Fighter Regiment, Vietnam People’s Air Force. They ejected but were captured. Both men were held as Prisoners of War until 4 March 1973.
Colonel Leo Keith Thorsness, United States Air Force (Retired) died Tuesday, 2 May 2017, at St. Augustine, Florida. He was 85 years of age.
