Lieutenant Commander William T. Amen, U.S. Navy, Commanding Officer of Fighter Squadron VF-111, is congratulated on his air to air victory after returning to the aircraft carrier USS Philippine Sea (CV-47). (U.S. Navy)
9 November 1950: The first jet vs. jet air-to-air victory which can be confirmed from both sides occurred when Lieutenant Commander William T. Amen, United States Navy, flying a Grumman F9F-2B Panther, Bu. No. 127184, shot down a Soviet Mikoyan-Gurevich MiG-15 over Korea.
Captain Mikhail Fedorovich Grachev, 139th Guards Fighter Aviation Regiment, led a squadron of MiG-15 fighters from their base at Antung, China to intercept U.S. Navy Douglas AD Skyraiders which were attacking bridges across the Yalu River, which marked the border between China and Korea.
Russian technicians service a MiG-15bis of the 351st Fighter Aviation Regiment at Antung Air Base, China, mid-1952. (Unattributed)
An escorting group of Grumman F9F-2B Panther fighters, assigned to Fighter Squadron 111 (VMF-111, “Sundowners”) aboard the Essex-class aircraft carrier, USS Philippine Sea (CV-47) went after the MiGs as they dove on the Skyraiders. The Soviet flight broke up into single aircraft, or pairs, and did not counterattack with any organization. Visibility was poor, and airplanes would disappear then reappear in the clouds.
Captain Grachev made a quick left turn, then reversed and rolled over into a dive. His two wingmen could not stay with him and visual contact was lost.
Bill Amen saw Grachev’s diving MiG-15 and, following him down, fired his four 20 mm cannon. Amen’s wingman saw the MiG crash into a wooded slope and burn. Grachev did not return from his mission and is presumed to have been killed in the crash.
USS Philippine Sea (CV-47) with Douglas AD Skyraiders and Grumman F9F Panthers on the flight deck, off the coast of Korea. Philippine Sea was a “long-hull” Essex-class ship, sometimes called the Ticonderoga-class. (U.S. Navy)
The Grumman F9F-2 Panther was a single-seat, single-engine turbojet powered fighter designed for operation from the U.S. Navy’s aircraft carriers. It was 38 feet, 5⅜ inches (11.719 meters) long, with a wingspan of 38 feet, 0 inches (11.528 meters)— not including wing tanks. Its overall height was 11 feet, 4 inches (3.454 meters). The wings could be hydraulically folded to reduce the span for storage aboard ship. The Panther weighed 9,303 pounds (4,220 kilograms) empty, and had a gross weight of 19,494 pounds (8,842 kilograms).
The F9F-2 was powered by a Pratt & Whitney Turbo Wasp JT6 (J42-P-8) turbojet engine which produced 5,000 pounds of thrust (22.241 kilonewtons) at Sea Level. The J42 was a license-built version of the Rolls-Royce Nene. The engine used a single-stage centrifugal-flow compressor, 9 combustion chambers and a single-stage axial-flow turbine. The engine weighed 1,715 pounds (778 kilograms).
Interestingly, the MiG-15 was powered by an un-licensed, reverse-engineered version of the Nene, the Klimov VK-1.
The Panther had a maximum speed of 575 miles per hour (925 kilometers per hour) at Sea Level. Its service ceiling was 44,600 feet (13,594 meters), and the range was 1,353 miles (2,177 kilometers).
The Panther was armed with four M3 20 mm autocannon placed in the nose, with 760 rounds of ammunition. It could carry up to 3,000 pounds (1,361 kilograms) of bombs or eight 5-inch (12.7 centimeters) rockets on four hardpoints under each wing.
The XF9F-2 prototype first flew 21 November 1947. 1,382 were produced and remained in service with the U.S. Navy and Marine Corps until 1958. A swept wing version, the F9F-6 through F9F-9J Cougar, was also produced.
For his service with VF-111 in combat from 5 August 1950 to 1 February 1951, Lieutenant Commander Amen was awarded the Distinguished Flying Cross.
F9F-2 Bu. No. 127184 was part of a group of 28 Grumman F9F panthers that were sold to the Argentine Navy. It was transferred in April 1963.
A Grumman F9F-2 Panther of Fighter Squadron 111 drops bombs over Korea, circa 1952. It is painted overall Glossy Sea Blue with red accents at the nose and tail. This is similar in appearance to the Panther flown by Lieutenant Commander William T. Amen, 9 November 1950. (U.S. Navy)
1st Lieutenant Donald Joseph Gott, Air Corps, Army of the United States. (American Air Museum in Britain UPL-71688)
MEDAL OF HONOR
DONALD JOSEPH GOTT
Rank and organization: 1st Lieutenant, United States Army Air Forces, 729th Bombardment Squadron, 452nd Bombardment Group Place and date: Saarbrücken, Germany, 9 November 1944. Entered service at: Arnett, Oklahoma. Born: 3 June 1923, Arnett, Oklahoma.
War Department, General Order No. 38, 16 May 1945
Citation:
The President of the United States of America, in the name of Congress, takes pride in presenting the Medal of Honor (Posthumously) to First Lieutenant (Air Corps) Donald Joseph Gott (ASN: 0-763996), United States Army Air Forces, for conspicuous gallantry and intrepidity in action above and beyond the call of duty while serving with the 729th Bombardment Squadron, 452d Bombardment Group (H), Eighth Air Force in action over Saarbrucken, Germany, on 9 November 1944. On a bombing run upon the marshaling yards at Saarbrucken a B-17 aircraft piloted by First Lieutenant Gott was seriously damaged by anti-aircraft fire. Three of the aircraft’s engines were damaged beyond control and on fire; dangerous flames from the No. 4 engine were leaping back as far as the tail assembly. Flares in the cockpit were ignited and a fire raged therein, which was further increased by free-flowing fluid from damaged hydraulic lines. The interphone system was rendered useless. In addition to these serious mechanical difficulties the engineer was wounded in the leg and the radio operator’s arm was severed below the elbow. Suffering from intense pain, despite the application of a tourniquet, the radio operator fell unconscious. Faced with the imminent explosion of his aircraft, and death to his entire crew, mere seconds before bombs away on the target, First Lieutenant Gott and his copilot conferred. Something had to be done immediately to save the life of the wounded radio operator. The lack of a static line and the thought that his unconscious body striking the ground in unknown territory would not bring immediate medical attention forced a quick decision. First Lieutenant Gott and his copilot decided to fly the flaming aircraft to friendly territory and then attempt to crash land. Bombs were released on the target and the crippled aircraft proceeded alone to Allied-controlled territory. When that had been reached, First Lieutenant Gott had the copilot personally inform all crewmembers to bail out. The copilot chose to remain with 1st. Lieutenant Gott in order to assist in landing the bomber. With only one normally functioning engine, and with the danger of explosion much greater, the aircraft banked into an open field, and when it was at an altitude of 100 feet it exploded, crashed, exploded again and then disintegrated. All three crewmembers were instantly killed. First Lieutenant Gott’s loyalty to his crew, his determination to accomplish the task set forth to him, and his deed of knowingly performing what may have been his last service to his country was an example of valor at its highest.
2nd Lieutenant William E. Metzger, Jr., Air Corps, Army of the United States
MEDAL OF HONOR
WILLIAM EDWARD METZGER, JR.
Rank and organization: 2nd Lieutenant, United States Army Air Forces, 729th Bombardment Squadron, 452nd Bombardment Group (H) Place and date: Saarbrücken, Germany, 9 November 1944. Entered service at: Lima, Ohio. Born: 9 February 1922, Lima, Ohio.
General Orders: War Department, General Orders No. 38 (May 16, 1945)
Citation:
The President of the United States of America, in the name of Congress, takes pride in presenting the Medal of Honor (Posthumously) to Second Lieutenant (Air Corps) William Edward Metzger, Jr. (ASN: 0-558834), United States Army Air Forces, for conspicuous gallantry and intrepidity in action above and beyond the call of duty while serving with the 729th Bombardment Squadron, 452d Bombardment Group (H), Eighth Air Force. On a bombing run upon the marshaling yards at Saarbrucken, Germany, on 9 November 1944, a B-17 aircraft on which Second Lieutenant Metzger was serving as copilot was seriously damaged by anti-aircraft fire. Three of the aircraft’s engines were damaged beyond control and on fire; dangerous flames from the No. 4 engine were leaping back as far as the tail assembly. Flares in the cockpit were ignited and a fire roared therein which was further increased by free-flowing fluid from damaged hydraulic lines. The interphone system was rendered useless. In addition to these serious mechanical difficulties the engineer was wounded in the leg and the radio operator’s arm was severed below the elbow. Suffering from intense pain, despite the application of a tourniquet, the radio operator fell unconscious. Faced with the imminent explosion of his aircraft and death to his entire crew, mere seconds before bombs away on the target, Second Lieutenant Metzger and his pilot conferred. Something had to be done immediately to save the life of the wounded radio operator. The lack of a static line and the thought that his unconscious body striking the ground in unknown territory would not bring immediate medical attention forced a quick decision. Second Lieutenant Metzger and his pilot decided to fly the flaming aircraft to friendly territory and then attempt to crash land. Bombs were released on the target and the crippled aircraft proceeded along to Allied-controlled territory. When that had been reached Second Lieutenant Metzger personally informed all crewmembers to bail out upon the suggestion of the pilot. Second Lieutenant Metzger chose to remain with the pilot for the crash landing in order to assist him in this emergency. With only one normally functioning engine and with the danger of explosion much greater, the aircraft banked into an open field, and when it was at an altitude of 100 feet it exploded, crashed, exploded again, and then disintegrated. All three crewmembers were instantly killed. Second Lieutenant Metzger’s loyalty to his crew, his determination to accomplish the task set forth to him, and his deed of knowingly performing what may have been his last service to his country was an example of valor at its highest.
The wounded man for whom Lieutenants Gott and Metzger sacrificed their lives was the bomber’s radio operator, Technical Sergeant Robert Alexander Dunlap, of Fresno, California. Unknown to the two pilots, the tail gunner, Staff Sergeant Herman Bruce Krimminger, from Charlotte, North Carolina, had become entangled in the airplane’s tail section. He was also killed in the crash.
Aviation Cadet Donald Joseph Gott, United States Army Air Force. (U.S. Air Force)
Donald Joseph Gott was born 3 June 1923, on a family farm 12 miles (19 kilometers) northeast of Arnett, Oklahoma. He was the fifth child of Joseph Eugene Gott, a farmer, and Mary Lucy Hanlon Gott. He attended Fargo High School, Fargo, Oklahoma, graduating in 1939.
In 1942, when Gott registered for Selective Service (conscription), he lived in Bridgeport, Connecticut, and was employed by the United States Aluminum Company. He had brown hair, blue eyes, a light complexion, was 5 feet, 7½ inches (171.45 centimeters) tall and weighed 150 pounds (68 kilograms).
On 21 September 1942, Donald Gott joined the Enlisted Reserve Corps. He began flight training as an aviation cadet in March 1943.
Donald Joseph Gott was commissioned as a second lieutenant, Air Corps, Army of the United States, 6 January 1944.
The 9 November 1944 mission was Gott’s fortieth combat mission. He had ten more to complete the fifty missions required for a combat tour by that stage of the war.
The Medal of Honor was presented to Lieutenant Gott’s mother by Major General Robert Boyd Williams ¹ during a ceremony at Fargo High School, 18 June 1945. In addition to the Medal of Honor, Gott was posthumously awarded the Purple Heart and the Air Medal with three oak leaf clusters (four awards).
Lieutenant Gott’s remains were initially buried at a temporary U.S. Army cemetery at Limey, Meurthe-et Moselle, France, along with those of Technical Sergeant Robert A. Dunlap and Staff Sergeant Herman B. Krimminger, but later removed and reburied at the Harmon Cemetery, Harmon, Oklahoma.
Aviation Cadet William Edward Metzger, Jr., Air Corps, Army of the United States. (United States Air Force)
William Edward Metzger, Jr., was born 9 February 1922 in Allen County, Ohio. He was the second of five children of William Edward Metzger, a real estate agent, and Ethel V. Badeau Metzger. He attended the Lima Central High School, and after graduation, was employed by the Lima Electric Motor Company.
Metzger registered for Selective Service (conscription) on 27 June 1942. He was described as having brown hair, blue eyes and a light complexion, was 5 feet 7 inches (170.18 centimeters) tall and weighed 150 pounds (68 kilograms).
Metzger enlisted in the United States Army as a private, 5 October 1942, at Toledo, Ohio. He served at Camp Perry, Ohio, and at the Desert Training Center, Camp Young,² near the Chiriaco Summit in the Colorado Desert of southern California. Private Metzger was next assigned as an aviation cadet. He began flight training in March 1943.
William Edward Metzger, Jr., was commissioned as a second lieutenant, Air Corps, Army of the United States, 21 August 1944.
Major General Frederick L. Anderson, Jr., Assistant Chief of Staff, United States Army Air Forces (formerly, commanding general, VIII Bomber Command), presented the Medal of Honor to Lieutenant Metzger’s parents during a ceremony held at the Market Street Presbyterian Church, Lima, Ohio, 17 June 1945. He was also awarded the Purple Heart, and the Air Medal with three oak leaf clusters (four awards).
Along with 1st Lieutenant Gott, Sergeants Dunlap and Krimminger, Lieutenant Metzger’s remains were buried at the temporary U.S. Army cemetery at Limey, Meurthe-et Moselle, France. His remains were later removed and reburied at Woodlawn Cemetery, Lima, Ohio, 30 August 1948.
Sergeant Dunlap’s remains were later interred at the Lorraine American Cemetery, St. Avoid, France. He was posthumously awarded the Purple Heart, and previously, the Air Medal with two oak leaf clusters (three awards).
Vega B-17G-35-VE Flying Fortress 42-97904, “Lady Jeanette,” photographed over Stuttgart, Germany, 5 September 1944. (American Air Museum in Britain, Roger Freeman Collection, FRE 1822)
Vega Aircraft Corporation B-17G-35-VE Flying Fortress 42-97904 (s/n 17-7269) was accepted by the United States Army Air Forces at Lockheed Field, Burbank, California, in March 1944. It was delivered to the Douglas Aircraft Modification Center (Air Force Plant #3) at Tulsa, Oklahoma, 31 March 1944. The bomber was then transferred to Kearney Army Airfield, a processing field for B-17 aircraft and their crews, 5 miles (8 kilometers) northeast of Kearney, Nebraska, 29 May, 1944. It was flown to Dow Field, Bangor, Maine, 6 June 1944, for ferrying across the North Atlantic Ocean. 42-97904 was damaged while taxiing at RCAF Gander Field, Newfoundland, where it had stopped to refuel on that same day. On arrival in England, 7 June 1944, -904 was assigned to the 452nd Bombardment Group (Heavy) at RAF Deopham Green (USAAF Station 142), 2 miles (3.2 kilometers) north of Attleborough, Norfolk, England. The bomber was originally nicknamed Why Worry, but this was later changed to Lady Jeanette.
The B-17G was the final production variant of the Flying Fortress. It entered service with the United States Army Air Forces in 1943.
The Boeing B-17G Flying Fortress was a four-engine heavy bomber operated by a combat crew of nine to ten men. It was 74 feet, 8.90 inches (22.781 meters) long with a wingspan of 103 feet, 9.38 inches (31.633 meters) and an overall height of 19 feet, 1.00 inch (5.187 meters). The wings have 3½° angle of incidence and 4½° dihedral. The leading edges are swept aft 8¾°. The total wing area is 1,426 square feet (132.48 square meters). The horizontal stabilizer has a span of 43 feet (13.106 meters) with 0° incidence and dihedral. Its total area, including elevators, is 331.1 square feet (12.18 square meters). The B-17G had an empty weight of 35,972 pounds (16,316.6 kilograms), and the maximum takeoff weight was 67,860 pounds (30,780.8 kilograms).
The B-17G was powered by four air-cooled, supercharged, 1,823.129-cubic-inch-displacement (29.876 liters) Wright Cyclone C9GC (R-1820-97) nine-cylinder radial engines with a compression ratio of 6.70:1. The engines were equipped with remote General Electric turbochargers capable of 24,000 r.p.m. The R-1820-97 had a Normal Power rating of 1,000 horsepower at 2,300 r.p.m. at 25,000 feet (7,620 meters), and 1,200 horsepower at 2,500 r.p.m. for Takeoff and Military Power. The engine could produce 1,380 horsepower at 2,500 r.p.m., War Emergency Power. 100-octane aviation gasoline was required. The Cyclones turned three-bladed, constant-speed, Hamilton Standard Hydromatic propellers with a diameter of 11 feet, 7 inches (3.835 meters) through a 0.5625:1 gear reduction. The R-1820-97 engine was 3 feet, 11.80 inches (1.214 meters) long and 4 feet, 7.10 inches (1.400 meters) in diameter, and weighed 1,315 pounds (596 kilograms).
The B-17G had a cruising speed of 172 knots (198 miles per hour/319 kilometers per hour) at 10,000 feet (3,048 meters). The maximum speed was 285 knots (328 miles per hour/528 kilometers per hour) at 26,700 feet (8,138 meters). The service ceiling was 38,450 feet (11,720 meters) at maximum power.
The B-17G had a fuel capacity of 2,780 gallons (10,523 liters) in twelve wing tanks. Two “Tokyo tanks” could be installed in the bomb bay, increasing capacity by 820 gallons (3,104 liters). The B-17G combat radius of 689 nautical miles (793 statute miles/1,276 kilometers) with max bomb load, and a maximum ferry range of 2,624 nautical miles (3,031 statute miles/4,878 kilometers).
The B-17G was armed with thirteen Browning AN-M2 .50-caliber machine guns for defense against enemy fighters. Power turrets mounting two guns each were located at the nose, dorsal, and ventral positions. Two guns could be installed in flexible mounts in the nose compartment, one in the radio compartment, two in the waist and two in the tail. 5,970 rounds of ammunition were carried.
The maximum bomb load of the B-17G was 12,800 pounds (5,806 kilograms). The internal bomb bay could be loaded with a maximum of six 1,000-pound general purpose bombs, or ten 1,000-pound armor piercing bombs; eight 1,600-pound (725.75 kilogram) armor piercing bombs; or two 2,000-pound general purpose bombs. The physical size of e
type limited the number that could be carried in the bomb bay. A 4,000-pound bomb could be carried on each of the bombers two underwing bomb racks.
The B-17 Flying Fortress was in production from 1936 to 1945. 12,731 B-17s were built by Boeing, Douglas Aircraft Com
pany and Lockheed-Vega. (The manufacturer codes -BO, -DL and -VE follows the Block Number in each airplane’s type designation.) 8,680 of these were B-17Gs, with 4,035 built by Boeing, 2,395 by Douglas and 2,250 by Lockheed-Vega.
¹ General Williams led the raid against the ball bearing factories at Schweinfurt, Germany,17 August 1943.
² Camp Young was the headquarters of General George S. Patton’s 3rd Armored Division.
Boeing XC-97 43-27470, the first of three Model 367 prototypes. (San Diego Air and Space Museum Archive)
9 November 1944: Boeing’s senior test pilot, Albert Elliott Merrill, and co-pilot John Bernard Fornasero make the first flight of the Boeing Model 367 prototype, XC-97 43-27470.
The airplane was a prototype for a very long range military transport. It used the wings, engines and tail of the B-29 Superfortress heavy bomber.
Boeing XC-97 three-view illustration with dimensions. (Warbird Information Exchange)
The three XC-97 prototypes were 110 feet, 4 inches (33.630 meters) long with a wingspan of 141 feet, 2.76 inches (43.0469 meters) and overall height of 33 feet, 2.8 inches (10.130 meters).
The production C-97A first flew in 1949. It used the more powerfull engines and taller vertical fin of the B-50 Superfortress. The transport had a flight crew of five and could carry 134 troops or 83 litters. The Stratofreighter’s empty weight was 76,143 pounds (34,538 kilograms) and maximum takeoff weight of 175,000 pounds (79,379 kilograms). The maximum cargo capacity was 67,080 pounds (30,427 kilograms).
The KC-97A had a maximum speed of 334 knots (384 miles per hour, or 619 kilometers per hour) at 26,000 feet (7,925 meters). Its ceiling was 34,500 feet (10,516 meters) and the airplane’s combat range was 1,661 nautical miles (1,911 statute miles/3,076 kilometers).
Boeing built 888 C-97 Stratofreighters and KC-97 Stratotankers between 1947 and 1958. The type was finally retired from the U.S. Air Force in 1978. Another 56 Model 377 Stratocruiser civil transports were produced.
This painting by famed aviation artist Keith Ferris depicts 1st Lieutenant Russell Brown’s Lockheed F-80C Shooting Star as he shot down an enemy Mikoyan-Gurevich MiG 15 over Korea, 8 November 1950. (Keith Ferris)
8 November 1950: First Lieutenant Russell J. Brown, United States Air Force, 16th Fighter Interceptor Squadron, 51st Fighter Interceptor Wing, is credited with shooting down a Russian-built Mikoyan-Gurevich MiG 15 jet fighter near the Yalu River while flying a Lockheed F-80C-10-LO Shooting Star. This may have been the very first time that a jet fighter had been shot down by another jet fighter.
Sources vary, reporting the serial number of Lieutenant Brown’s fighter as 49-713 or 49-717.
A contemporary newspaper quoted Brown:
1st Lieutenant Russell J. Brown. (Air Force Times)
Brown gave a colorful description of the fight in history’s first jet-versus-jet battle last week. He said:
“We had just completed a strafing run on Sinuiju antiaircraft positions and were climbing when we got word that enemy jets were in the area.
“Then we saw them across the Yalu, doing acrobatics.
“Suddenly they came over at about 400 miles an hour. We were doing about 300. They broke formation right in front of us at about 18,000 or 20,000 feet. They were good looking planes—shiny and brand, spanking new.”
—INS, Tokyo, November 13
Soviet records reported no MiG 15s lost on 8 November. Senior Lieutenant Kharitonov, 72nd Guards Fighter Aviation Unit, reported being attacked by an F-80 under circumstances that suggest this was the engagement reported by Lieutenant Brown, however Kharitonov succeeded in evading the American fighter after diving away and jettisoning his external fuel tanks.
A Soviet MiG 15 pilot, Lieutenant Khominich, also of the 72nd Guards, claimed shooting down an American F-80 on 1 November, but U.S. records indicate that this fighter had been destroyed by anti-aircraft fire.
What is clear is that air combat had entered the jet age, and that the Soviet Union was not only supplying its swept wing MiG 15 to North Korea and China, but that Soviet Air Force pilots were actively engaged in the war in Korea.
Russian technicians service a MiG 15bis of the 351st IAP at Antung Air Base, China, mid-1952. (Unattributed)
The Mikoyan-Gurevich MiG 15 is a single-seat, single engine turbojet-powered fighter interceptor, designed to attack heavy bombers. Designed for high sub-sonic speed, the leading edges of the wings and tail surfaces were swept to 35°. The wings were very thin to minimize aerodynamic drag.
The fighter was 10.102 meters (33 feet, 1.7 inches) long, with a wingspan of 10.085 meters (33 feet, 1 inch). Its empty weight was 3,253 kilograms (7,170 pounds) and takeoff weight was 4,963 kilograms (10,938 pounds).
The Rolls-Royce Nene I and Nene II jet engines had been used in the three MiG 15 prototypes. The British engines were reverse-engineered by Vladimir Yakovlevich Klimov and manufactured at Factory No. 45 in Moscow as the Klimov VK-1. The VK-1 used a single-stage centrifugal-flow compressor, 9 combustion chambers and a single-stage axial-flow turbine. It produced a maximum 26.5 kilonewtons of thrust (5,957 pounds of thrust). The VK-1 was 2.600 meters (8 feet, 6.4 inches) long, 1.300 meters (4 feet, 3.2 inches) in diameter, and weighed 872 kilograms (1,922 pounds).
The MiG 15 had a maximum speed of 1,031 kilometers per hour (557 knots/641 miles per hour) at 5,000 meters (16,400 feet) and 1,050 kilometers per hour (567 knots/652 miles per hour) at Sea Level.
Armament consisted of one Nudelman N-37 37 mm cannon and two Nudelman-Rikhter NR-23 23 mm cannon.
MIG 15 Red 2057. A North Korean Peoples’ Air Force Mikoyan-Gurevich MiG 15bis in a hangar at Kimpo Air Base, Republic of South Korea. A defecting North Korean pilot, Lieutenant No Kum-Sok, flew it to Kimpo on 21 September 1953. It was taken to Okinawa, examined and test flown by U.S.A.F. test pilots, including Major Charles E. (“Chuck”) Yeager. This MiG 15 is in the collection of the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio. (U.S. Air Force).
The Lockheed P-80 Shooting Star was the United States’ first operational jet fighter. It was redesignated F-80 in 1948. It was a single-seat, single-engine airplane, designed by a team of engineers led by Clarence L. (“Kelly”) Johnson. The prototype XP-80A, 44-83020, nicknamed Lulu-Belle, was first flown by test pilot Tony LeVier at Muroc Army Air Field (now known as Edwards Air Force Base) 8 January 1944. The P-80A entered production in 1945. Improved versions, the P-80B and P-80C (F-80C) followed.
Lockheed F-80C-10-LO Shooting Star 49-432 on display at the Air Force Armaments Museum, Eglin Air Force Base, Florida. The fighter is marked as F-80C-10-LO 49-713, assigned to the 16th Fighter Squadron, 51st Fighter Interceptor Group, Kimpo, Korea, 1950.
The F-80C was 34 feet, 5 inches (10.490 meters) long with a wingspan of 38 feet, 9 inches (11.811 meters) and an overall height of 11 feet, 3 inches (3.429 meters). It weighed 8,420 pounds empty (3,819 kilograms) and had a maximum takeoff weight of 16,856 pounds (7,645 kilograms).
The F-80C was powered by either a General Electric J33-GE-11, Allison J33-A-23 or J33-A-35 turbojet engine. The J33 was a development of an earlier Frank Whittle-designed turbojet. It used a single-stage centrifugal-flow compressor, eleven combustion chambers and a single-stage axial-flow turbine section. The J33-A-35 had a Normal Power rating of 3,900 pounds of thrust (17.348 kilonewtons) at 11,000 r.p.m., at Sea Level, and 4,600 pounds (20.462 kilonewtons) at 11,500 r.p.m., for Takeoff. It was 107 inches (2.718 meters) long, 50.5 inches (1.283 meters) in diameter, and weighed 1,820 pounds (826 kilograms).
The F-80C had a maximum speed of 594 miles per hour (516 knots/956 kilometers per hour) at Sea Level and 543 miles per hour (472 knots/874 kilometers per hour) at 25,000 feet (7,620 meters). The service ceiling was 46,800 feet (14,265 meters). The maximum range was 1,380 miles (2,221 kilometers).
The F-80C Shooting Star was armed with six Browning AN-M3 .50-caliber aircraft machine guns mounted in the nose.
A Lockheed F-80C Shooting Star of the 16th Fighter Interceptor Squadron, 51st Fighter Interceptor Wing, makes a JATO-assisted takeoff from an airfield in the Republic of South Korea, circa 1950. (U.S. Air Force)
Lockheed F-80C-10-LO Shooting Star 49-713, flown by Albert C. Ware, Jr., was lost 10 miles north of Tsuiki Air Base, Japan, 23 March 1951.
Sir Charles Edward Kingsford Smith, M.C., A.F.C. (National Archives of Australia, A1200, L93634)
On 8 November 1935: Sir Charles Edward Kingsford Smith, M.C., A.F.C., and co-pilot John Thompson Pethybridge disappeared while flying Lady Southern Cross, a Lockheed Altair 8D Special, across the Andaman Sea from Allahabad, Indian Empire, to Singapore, Straits Settlements, a distance of approximately 1,932 nautical miles (2,224 statute miles, or 3,578 kilometers). The aviators were attempting to break a speed record for flight from England to Australia.
The airplane was sighted over Calcutta, British India, at 9:06 a.m., local time.
The pilot of another airplane, Charles James (“Jimmy”) Melrose, who was also en route to Australia, reported that,
“. . . he saw a ‘plane, which must have been Kingsford Smith’s, pass about 200 feet above him at 3 o’clock this morning, when he was over the Bay of Bengal, about 150 miles from land. . . Mr. Melrose said that when he passed over him in the Bay of Bengal Kingsford Smith’s speed was double his own, which was 110 miles an hour. It gave him an uncanny feeling over the desolate ocean to see the spurts of flame coming from the twin exhausts of the Lady Southern Cross. . . Kingsford Smith’s altitude was between 8000 and 9000 feet.”
—The Sydney Morning Herald, No. 30,531, Saturday, 9 November 1935, Page 19, Columns 7 and 8
On 1 May 1937, about eighteen months after the disappearance, two Burmese fisherman found a landing gear assembly floating in the Andaman Sea near Kokunye Kyun (Aye Island), off the west coast of Burma. Lockheed was able to confirm that it was from Lady Southern Cross. The component is in the collection of the Powerhouse Museum, Sydney, Australia.
Landing gear assembly of Kingsford Smith’s Lady Southern Cross is in the collection of the Powerhouse Museum venue of the Museum of Applied Arts and Sciences. (MAAS Collection 94/64/1)
In 2009, searchers claimed to have located the wreck of the airplane near the island, but this has not been confirmed.
Lockheed Altair 8D Special VH-USB, Lady Southern Cross, at Burbank, California, September 1935. The Altair is “. . . painted consolidated blue with silver wing and silver striping. . . .” (David Horn Collection No. 9099)
Kingsford Smith was a former Royal Air Force pilot and flight instructor. He had been a barnstormer, airline pilot, and gained world-wide fame for his trans-Pacific flights. From 31 May to 9 June 1928 he and Charles Ulm, Harry Lyon and James Warner had flown Southern Cross, a Fokker F.VIIB/3m, from Oakland, California to Brisbane, with stops at Hawaii and Fiji. In 1934, with Lady Southern Cross, he and Patrick Gordon Taylor flew from Australia to Hawaii and on to Oakland, California, arriving 4 November.
Charles Kingsford Smith’s Lady Southern Cross at Lockheed, Burbank, California. Note the navigator’s sighting lines on the elevators. (Code One Magazine/Lockheed Martin)
After the transpacific flight, Lady Southern Cross spent the next 11 months at Lockheed being repaired and overhauled. Kingsford Smith then flew it across the United States and had it transported to England aboard a ship.
Lady Southern Cross was a Lockheed Altair 8D Special, a single-engine monoplane with the fuselage, wings and tail surfaces built of spruce. The Altair had been modified from a 1930 Lockheed Sirius 8A Special, NR118W, c/n 152, which was an airplane with fixed landing gear. Lockheed designed a new wing which included retractable landing gear, operated by a hand crank from the cockpit. The Sirius and Altair were single-place utility transports. Kingsford Smith’s Altair was further modified with two cockpits in tandem. Lady Southern Cross was painted Consolidated Blue (a dark blue color) with silver accents.
Air Commodore Sir Charles Edward Kingsford Smith, Kt, MC, AFC, with the Lady Southern Cross at Croydon, 17 October 1935. The airplane’s registration has been changed to G-ADUS. (PHOTOSHOT)
Lady Southern Cross had a length of 27 feet, 10 inches (8.484 meters) with a wingspan of 42 feet, 9¼ inches (13.037 meters) and height of 9 feet, 3 inches (2.819 meters). The modified airplane had an empty weight of 3,675 pounds (1,667 kilograms) and a maximum gross weight of 6,700 pounds (3,039 kilograms).
The airplane’s standard Pratt & Whitney Wasp C1 engine was replaced at Kingsford Smith’s request with a more-powerful Pratt & Whitney Wasp SE, serial number 5222. The Wasp SE was an air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) single-row 9-cylinder radial engine with a compression ratio of 6:1. It was rated at 500 horsepower at 2,200 r.p.m., at an altitude of 11,000 feet (3,353 meters). The SE was a direct-drive, right-hand tractor engine which turned a two-bladed Hamilton Standard controllable-pitch metal propeller with a diameter of 9 feet, 0 inches (2.743 meters). The Wasp SE was 3 feet, 6.59 inches (1.082 meters) long, 4 feet, 3.44 inches (1.307 meters) in diameter and weighed 750 pounds (340.2 kilograms).
An Altair 8D had a cruising speed of 175 miles per hour (282 kilometers per hour) and a maximum speed of 207 miles per hour (333 kilometers per hour) at 7,000 feet (2,134 meters). Contemporary news reports stated that Kingsford Smith had reached speeds of 230 miles per hour (370 kilometers per hour) while testing VH-USB.
Air Commodore Sir Charles Edward Kingsford Smith, Kt, MC, AFC, at Lympne Airport, Kent, England, 6 November 1935. This may be the last photograph ever taken of “Smithy.” (International News Photos)
