Lieutenant Henry A. Johnson, USAAF, with Lockheed P-80A-1-LO Shooting Star 44-85123. (FAI)
3 June 1946: Lieutenant Henry A. Johnson, U.S. Army Air Force, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 1,000 Kilometers Without Payload flying a Lockheed P-80A-1-LO Shooting Star, serial number 44-85123, at Dayton, Ohio. The average speed was 745.08 kilometers per hour (462.97 miles per hour). The elapsed time was 1 hour, 20 minutes, 31 seconds.¹
This airplane had earlier set a transcontinental speed record when Colonel William H. Councill flew it from Daugherty Field, Long Beach, California to La Guardia Field, New York, in 4 hours, 13 minutes, 26 seconds on 26 January 1946. It would go on to win the Thompson Trophy Race J Division, 2 September 1946, when Major Gustav E. Lundquist flew it to an average speed of 515.853 miles per hour (830.185 kilometers per hour) over the 180-kilometer course.
Lockheed P-80A-1-LO 44-85123, photographed 22 June 1946 at the General Electric Air Research Laboratory, Schenectady, New York, by Richard Lockett. (Brian Lockett/Air-and-Space.com)
The Lockheed P-80-1-LO was the United States’ first operational jet fighter. 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 AFB) 8 January 1944.
The P-80A was 34 feet, 6 inches (10.516 meters) long with a wingspan of 38 feet, 10.5 inches (37 feet, 7.5 inches with “clipped” wing tips) (11.849 or 11.468 meters) and an overall height of 11 feet, 4 inches (3.454 meters). The wings had 1° incidence with -1° 30° twist, and 3° 50′ dihedral. The leading edges were swept aft 9° 18′ 33″. The total wing area was 237.70 square feet (22.08 square meters). The P-80A weighed 7,920 pounds empty (3,593 kilograms) and had a maximum takeoff weight of 14,000 pounds (6,350 kilograms).
Lockheed P-80A-1-LO Shooting Star 44-85123, World Speed Record Holder. (FAI)
Early production P-80As were powered by either an Allison J33-A-9 or a General Electric J33-GE-11 turbojet engine. The J33 was a licensed version of the Rolls-Royce Derwent. It was a single-shaft turbojet with a 1-stage centrifugal compressor section and a 1-stage axial-flow turbine. The -9 and -11 engines were rated at 3,825 pounds of thrust (17.014 kilonewtons) at 11,500 r.p.m. They were 8 feet, 6.9 inches (2.614 meters) long, 4 feet, 2.5 inches (1.283 meters) in diameter and weighed 1,775 pounds (805 kilograms).
The P-80A-1 had a maximum speed of 510 miles per hour (821 kilometers per hour) at Sea Level, 520 miles per hour (837 kilometers per hour) at 20,000 feet (6,096 meters), and 495 miles per hour (797 kilometers per hour) at 40,000 feet (12,192 meters). The service ceiling was 45,000 feet (13,716 meters).
Several hundred of the early production P-80 Shooting stars had all of their surface seams filled, and the airplanes were primed and painted. Although this process added 60 pounds (27 kilograms) to the empty weight, the decrease in drag allowed a 10 mile per hour (16 kilometers per hour) increase in top speed. The painted surface was difficult to maintain in the field and the process was discontinued.
The P-80A Shooting Star was armed with six Browning AN-M3 .50-caliber aircraft machine guns mounted in the nose, with 300 rounds of ammunition per gun.
44-85123 is undergoing restoration at Edwards Air Force Base, California.
Lockheed test pilots Anthony W. (“Tony”) LeVier and David L. Ferguson stand in front of P-80A 44-85123 and an F-117A Nighthawk at the Lockheed Skunk Works, Palmdale, California, 17 June 1993. (Denny Lombard, Lockheed Martin)
Captain Joseph W. Kittinger, Jr., U.S. Air Force, seated in the gondola of Project MANHIGH I, 2 June 1957. Captain Kittinger is wearing a slightly-modified David Clark Co. MC-3A capstan-type partial-pressure suit (S836) and ILC Dover MA-2 helmet for protection at very high altitudes. (U.S. Air Force)Project MANHIGH I balloon and gondola. (U.S. Air Force)
2 June 1957: At 6:23 a.m., Central Daylight Time (11:23 UTC), Captain Joseph W. Kittinger, Jr., United States Air Force, lifted off from Richard E. Fleming Field (SGS), South Saint Paul, Minnesota, in the gondola of a helium balloon designed and built by Winzen Research Inc.
At 8:04 a.m. (13:04 UTC), Captain Kittinger reached a pressure altitude of 95,000 feet (28,956 meters). This was only 400 feet (122 meters) short of the balloon’s theoretical pressure ceiling. Using U.S. Weather Bureau data, the linear altitude of the balloon was calculated to have been 97,000 feet (29,566 meters).¹
The Fédération Aéronautique Internationale (FAI) was not asked to certify this flight, so an official record was not set.
Project MANHIGH I was intended to test various equipment and human physiology in a near-space condition. Cosmic radiation was a particular concern. This was the first of many high-altitude research balloon flights that Kittinger would make.
. . . A Winzen crew conducted the launching, as provided by the Man-High contract, in collaboration with members of the Aeromedical Field Laboratory and other units at Holloman. The 475th Air Base Squadron, Minneapolis, provided additional helicopter support. The vehicle was a two-million-cubic-foot plastic balloon, 172.6 feet in diameter, which quickly reached the planned ceiling altitude of 95,000 feet, setting a new record for manned balloons. Test specifications called for a twelve-hour flight. However, because of an oxygen leak (due to an improperly connected valve) and also certain communications difficulties, Colonel Stapp and Mr. Winzen decided that Captain Kittinger should come down after not quite two hours at altitude. The balloon pilot was not happy with the decision, replying by radio, “Come and get me.” But he did come down, and landed successfully at 1257 hours none the worse for his experience.
— History of Research in Space Biology and Biodynamics, Part II, Chapter 3, NASA History Office, December 1958.
Kittinger landed next to a stream approximately 7 miles (11 kilometers) south-southwest of Alma, Minnesota. The total duration of his flight was 6 hours, 36 minutes. He was awarded the Distinguished Flying Cross, the first of six he would receive during his career in the Air Force.
Ground track of Project MANHIGH I balloon, 2 June 1957. (U.S. Air Force)
The Project MANHIGH balloon and gondola were designed and built by Winzen Research, Inc., South St. Paul, Minnesota. The gondola was used in all three MANHIGH flights (Kittinger, June 1957; Simons, August 1957; McClure, October 1958).
The balloon was constructed of polyethelene sheet with a thickness of 2 mils (0.002 inch/0.051 millimeter). The seams were bonded using a heat-sealing technique which had been developed by Otto Winzen. When fully inflated with helium, the envelope had a volume of 2,000,000 cubic feet (56,634 cubic meters) and diameter of 172.6 feet (52.6 meters).
Illustration of Project MANHIGH gondola. (U.S. Air Force)
The gondola is 8 feet high and 3 feet in diameter (2.4 × 0.9 meters). It consisted of a cast aluminum section with 6 portholes which served as the primary load-bearing unit of the gondola. The rest of the gondola consisted of an aluminum alloy cylinder and two hemispherical end caps. The capsule was pressurized and filled with a 60-20-20 mixture of oxygen, nitrogen, and helium.
The gondola was suspended from an open 40.4 foot (12.3 meter) diameter parachute, which was, in turn, attached the gas balloon’s suspension rigging. Four explosive devices could sever the attachments and release the gondola and parachute.
The balloon, parachute and associated equipment weighed 1,012 pounds (459 kilograms). The gondola and installed equipment weighed 598 pounds (271 kilograms) and carried another 246 pounds (112 kilograms) of used lead-acid batteries as ballast. Kittinger, with his personal equipment, food and water, added 240 pounds (109 kilograms) to the payload. Finally, there was 70 pounds (32 kilograms) of equipment for experiments, cameras and film. The total weight came to 2,166 pounds (982 kilograms).
The Project MANHIGH gondola is on display at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.
Project MANHIGH gondola at the National Museum of the United States Air Force. (U.S. Air Force)
Joe Kittinger flew three combat tours during the Vietnam War for a total of 483 combat missions. On 1 March 1972, flying a McDonnell Douglas F-4D Phantom II, he shot down an enemy Mikoyan-Gurevich MiG-21. He was himself shot down on 11 May 1972. He and his Weapons System Officer, 1st Lieutenant William J. Reich, were captured and spent 11 months at the Hanoi Hilton.
Captain Joseph W. Kittinger, Jr., United States Air Force. Captain Kittinger is wearing the wings of an Air Force Senior Pilot and an Air Force Basic Parachutist Badge. The red, white and blue striped ribbon represents the Distinguished Flying Cross. (U.S. Air Force)
Joe Kittinger holds six Fédération Aéronautique Internationale (FAI) world records for distance set with balloons. Three are still current.² In 2012, he was technical advisor for Felix Baumgartner as he set a new world record for the highest parachute jump from the Red Bull Stratos balloon and gondola. Kittinger died 9 December 2022.
Vera Winzen, founder and owner of Winzen Research, Inc. The Project MAN-HIGH gondola is in the background. (Joel Yale)
Winzen Research, Inc. was formed in 1949 by Otto Christian Winzen, an aeronautical engineer, and his wife, Vera M. Habrecht Winzen. Both were immigrants from Germany. Mr. Winzen had previously worked for the gas balloon laboratory of General Mills, Inc. Mrs. Winzen had borrowed money from her parents to start the company and held a 2/3 ownership of the company. She ran the factory and trained its workers. She also had four U.S. patents related to balloon construction.
Otto Christian Winzen was born 24 October 1917, at Cologne, Nordrhein-Westfalen, Germany. He was the son of Christian Winzen and Lilly Lerche Winzen. At the age of 19, Winzen sailed from Bremen, Germany, aboard the Norddeutsche Lloyd passenger liner S.S. Europa, on 29 June 1937. He arrived at New York City, New York, United States of America, on 5 July 1937.
Winzen studied aeronautical engineering at University of Detroit Mercy, a private Roman Catholic university in Detroit, Michigan. It was the first university to offer a complete 5-year degree program in aeronautical engineering. While there, he met the world famous aeronaut, Jean Felix Picard, and his future wife, Vera Habracht.
Reportedly, during World War II, Otto Winzen was interred as an enemy alien.
Otto Winzen later married Marion Grzyll. He committed suicide 23 November 1979 (the first Mrs. Winzen’s 59th birthday).
Major David G. Simons, M.D., U,S, Air Force, at left, with the Project MANHIGH gondola, Otto C. Winzen, and Vera M. Winzen (the future Mrs. Simons), circa 1957. (Photograph by Joel Yale/LIFE Photo Collection)
Wera Maria Habrecht was born 23 November 1920 at Heidenheim, Germany. She was the first of two children of Max Theodore Habrecht, a commercial photographer, and Maya Widenmann Habrecht. The family emigrated to the United States in 1923, with Mr. Habrecht traveling there first. Mrs. Habrecht followed later with her children, Wera and Roland. They first sailed from Hamburg, Germany, 13 November 1923, to the British seaport of Grimsby, Lincolnshire, aboard the passenger/cargo ship S.S. Dewsbury. On 16 Novemberl the family boarded S.S. Montlaurier at Liverpool, England, and then sailed for New York City. The Habrecht family settled in Detroit, Michigan.
Vera M. Habrecht, 1939. (The Triangle)
With her first name “americanized,” Vera M. Habrecht attended Cass Technical High School in Detroit, Michigan, graduating in 1939. She then studied art at the Walker Art Center and the Minneapolis School of Art, both in Minneapolis, Minnesota.
Miss Habrecht was introduced to Mr. Winzer by Professor Picard. They were married 1 February 1941, in Detroit.³ They divorced in 1958.
Mrs. Winzer was herself an aeronaut. In 1957 she competed in the 30th Annual International Gas Balloon Races in Holland.
During Project MANHIGH, she met Major David G. Simons, M.D., U.S.A.F. Major Simons flew the MANHIGH II mission, 19–20 August 1957. They were married 12 June 1959. It was the second marriage for both. This marriage also ended in divorce, 5 May 1969. Dr. Simons died 5 April 2010.
On 26 May 1975, she married her third husband, Clifford Charles La Plante, at Arlington, Virginia.
While conducting pollution research Mrs. La Plante, under the name Vera M. Simons, set a Comité International d’Aérostation (the FAI Ballooning Commission, or CIA, world record for the Longest Flight for a Female Pilot, at 133 hours, 45 minutes, 1 October 1979.⁴
Vera Maria Habrecht Winzer Simons La Plante died at Austin, Texas, 31 July 2012, at the age of 91 years.
Vera Simons with a gas balloon, Holland, 1975. (NASM)
¹ Air Force Missile Development Center Technical Report MANHIGH I, AFMDC-TR-59-24, Pages 33 and 35
² FAI Record File Numbers 1045, 1046, 1047
³ Some sources state that Mrs. Winzen had been married previously, and that she had a daughter from that marriage. TDiA has not found any information to support this claim.
1st Lieutenant John M. Conroy, 115th Fighter Interceptor Squadron, California Air National Guard, checks the time after arriving back at the point of departure, 21 May 1955. (Ralph Morse, LIFE Magazine, via Jet Pilot Overseas)
21 May 1955: At 05:59:45 Pacific Standard Time (13:59:45 UTC) 1st Lieutenant John M. (“Jack”) Conroy, U.S. Air Force, a World War II B-17 pilot and former Prisoner of War, took off from the California Air National Guard Base at the San Fernando Valley Airport (re-named Van Nuys Airport in 1957). His airplane was a specially-prepared North American Aviation F-86A-5-NA Sabre, USAF serial number 49-1046. His Destination? Van Nuys, California—by way of Mitchel Field, Long Island, New York. His plan was to return to the ANG base in “The Valley” before sunset.
North American Aviation F-86A-5-NA Sabre 49-1046, “California Boomerang.” (California State Military Museum)
Several weeks of planning and preparation were involved in “Operation Boomerang”. Five refueling stops would be required and Air National Guard personnel across the United States would handle that. A deviation from peacetime standards would allow the Sabre to be refueled with the engine running to minimize time spent on the ground. (The F-86 was not capable of inflight refueling.) The six-year-old F-86A was polished to ensure that all rivet heads were smooth, seams in the fuselage and wing skin panels were adjusted for precise fit, then were sealed. The gun ports for the six .50-caliber Browning machine guns in the fighter’s nose were filled then covered with doped fabric and painted. This was to reduce aerodynamic drag as much as possible. The General Electric J47-GE-13 turbojet was overhauled, then tested and adjusted for maximum efficiency.
Arrangements for official timing of the West to East and Back Again speed run were paid for by North American Aviation, Inc., whose personnel also provided technical support to the Air National Guard.
Jack Conroy’s F-86A was nicknamed California Boomerang, and had a map of the United States and a boomerang painted on the fuselage. The Sabre remained in its overall natural aluminum finish but had green stripes on the fuselage, vertical fin and wings.
North American Aviation F-86A-5-NA Sabre 49-1046, California Boomerang, being readied for its return flight at Mitchel Air Force Base, New York. (LIFE Magazine via Jet Pilot Overseas)
After takeoff, Lieutenant Conroy climbed to approximately 40,000 feet (12,192 meters) and headed to his first refueling stop at Denver, Colorado. He landed at 7:48 a.m. PST and the Sabre was refueled and off again in just 6 minutes. From Denver he continued eastward to Springfield, Illinois, arriving at 9:32 a.m. PST. Refueling there took 5 minutes. The next stop was Mitchel Field, Long Island, New York. He touched down at 11:19 a.m., PST and remained on the ground for 39 minutes.
Conroy departed Mitchel Field on the westbound leg at 11:58 a.m. PST and arrived at Lockburne Air Force Base, Ohio at 12:58 p.m., PST. This refueling stop required 7 minutes. Next on the flight plan was Tulsa, Oklahoma. The airplane landed there at 2:26 p.m. PST, and was refueled and airborne again in 6 minutes. The last refueling took place at Albuquerque, New Mexico. Lieutenant Conroy landed at 3:58 p.m., PST. After another 7 minute stopover, California Boomerang took off on the final leg of the round-trip journey, finally landing back at Van Nuys, California at 5:26:18 p.m., PST.
John Conroy’s Coast-to-Coast-to-Coast “dawn to dusk” flight covered 5,058 miles (8,140.1 kilometers). The total elapsed time was 11 hours, 26 minutes, 33 seconds. His average speed was 445 miles per hour (716.2 kilometers per hour). Weather across the country caused some delays as Jack Conroy had to make instrument approaches to three of the airports.
California Boomerang, 1st Lieutenant Jack Conroy’s California Air National Guard F-86A-5-NA Sabre, 49-1046, being “hot” refueled at an intermediate stop, 21 May 1951. At least six fueling hoses are simultaneously filling the fighter’s fuselage, wing and drop tanks tanks while the jet engine remains in operation. Note the fire fighting apparatus standing by in the background. (LIFE Magazine via Jet Pilot Overseas)
California Boomerang, North American Aviation F-86A-5-NA Sabre 49-1046, is on display as a “gate guard” at the entrance to the Channel Islands Air National Guard Station, adjacent to Naval Base Ventura County, Point Mugu, California.
North American Aviation F-86A Sabre 49-1046 at the entrance to the Channel Islands National Guard Station, Point Mugu, California. (Brian Lockett, Goleta Air and Space Museum)
20 May 1967: Colonel Robin Olds, USAF, commanding officer of the 8th Tactical Fighter Wing based at Ubon Rachitani Royal Thai Air Force Base, and Weapons System Officer 1st Lieutenant Stephen B. Croker, destroyed two Vietnam People’s Air Force MiG-17 fighters with AIM-7 Sparrow radar-guided and AIM-9 Sidewinder heat-seeking air-to-air missiles while flying McDonnell F-4C-24-MC Phantom II, serial number 64-0829, named SCAT XXVII.
An official U.S. Air Force history publication describes the air battle:
Two other MiG-17s became the victims of Col. Robin Olds and his pilot, 1st. Lt. Stephen B. Croker. [Note: at this point in time, the WSOs of USAF F-4Cs were fully-rated pilots.—TDiA] These were aerial victories three and four for Olds, making him the leading MiG-killer at that time in Southeast Asia. An ace from World War II, the 8th TFW commander was battle-tested and experienced. Olds termed the events of 20 May “quite a remarkable air battle.” According to his account:
F-105s were bombing along the northeast railroad; we were in escort position, coming in from the Gulf of Tonkin. We just cleared the last of the low hills lying north of Haiphong, in an east-west direction, when about 10 or 12 MiG-17s came in low from the left and, I believe, from the right. They tried to attack the F-105s before they got to the target.
Mikoyan Gurevich MiG-17F in Vietnam People’s Air Force markings at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio. (U.S. Air Force).
We engaged MiG-17s at approximately 15 miles short of the target. The ensuing battle was an exact replica of the dogfights in World War II.
Our flights of F-4s piled into the MiGs like a sledge hammer, and for about a minute and a half or two minutes that was the most confused, vicious dogfight I have ever been in. There were eight F-4Cs, twelve MiG-17s, and one odd flight of F-105s on their way out from the target, who flashed through the battle area.
Quite frankly, there was not only danger from the guns of the MiGs, but the ever-present danger of a collision to contend with. We went round and round that day with the battles lasting 12 to 14 minutes, which is a long time. This particular day we found that the MiGs went into a defensive battle down low, about 500 to 1,000 feet. In the middle of this circle, there were two or three MiGs circling about a hundred feet—sort of in figure-eight patterns. The MiGs were in small groups of two, three, and sometimes four in a very wide circle. Each time we went in to engage one of these groups, a group from the opposite side would go full power, pull across the circle, and be in firing position on our tails almost before we could get into firing position with our missiles. This was very distressing, to say the least.
The first MiG I lined up was in a gentle left turn, range about 7,000 feet. My pilot achieved a boresight lock-on, went full system, narrow gate, interlocks in. One of the two Sparrows fired in ripple guided true and exploded near the MiG. My pilot saw the MiG erupt in flame and go down to the left.
Colonel Robin Olds flew this McDonnell F-4C-24-MC Phantom II, 64-0829, SCAT XXVII, when he and 1st Lieutenant Stephen B. Croker shot down two VPAF MiG-17s near Haiphong, North Vietnam, 20 May 1967. (U.S. Air Force)
We attacked again, trying to break up that defensive wheel. Finally, once again, fuel considerations necessitated departure. As I left the area by myself, I saw that lone MiG still circling and so I ran out about ten miles and said that even if I ran out of fuel, he is going to know he was in a fight. I got down on the deck, about 50 feet, and headed right for him. I don’t think he saw me for quite a while. But when he did, he went mad, twisting, turning, dodging and trying to get away. I kept my speed down so I wouldn’t overrun him and I stayed behind him. I knew he was either going to hit that ridge up ahead or pop over the ridge to save himself. The minute he popped over I was going to get him with a Sidewinder.
I fired one AIM-9 which did not track and the MiG pulled up over the ridge, turned left and gave me a dead astern shot. I obtained a good growl. I fired from about 25 to 50 feet off the grass and he was clear of the ridge by only another 50 to 100 feet when the Sidewinder caught him.
The missile tracked and exploded 5 to 10 feet to the right side of the aft fuselage. The MiG spewed pieces and broke hard left and down from about 200 feet. I overshot and lost sight of him.
I was quite out of fuel and all out of missiles and pretty deep in enemy territory all by myself, so it was high time to leave. We learned quite a bit from this fight. We learned you don’t pile into these fellows with eight airplanes all at once. You are only a detriment to yourself.
— 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 59–60.
Colonel Robin Olds, 8th Tactical Fighter Wing, with SCAT XXVII, his McDonnell F-4C-24-MC Phantom II, 64-0829, at Ubon Rachitani RTAFB, 1967. U.S. Air Force)Fighter pilot Brigadier General Robin Olds, U.S. Air Force (Retired) with SCAT XXVII at the National Museum of the United States Air Force. General Olds died 14 June 2007. (U.S. Air Force)Robin Olds’ McDonnell F-4C-24-MC Phantom II, 64-0829, SCAT XXVII, at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Dayton, Ohio.
Sous-lieutenant Gervais Raoul Victor Lufbery, Aéronautique Militaire, circa 1917. Lufbery is wearing the pilot’s badge of the Aéronautique Militaire on his tunic. He also is wearing the Chevalier de la légion d’honneur, Médaille Militaire, and Croix de Guere with one silver and three bronze palms. The airplane is a Société Pour L’Aviation et ses Dérivés SPAD S.VII C.1 of Escadrille SPA 124, “La Fayette.” (Captain Robert Soubiran/Library of Congress LC-USZ62-101970)
19 May 1918: Major Gervais Raoul Victor Lufbery, 94th Aero Squadron, American Expeditionary Force, a leading Allied fighter pilot of World War I, was killed in action at Maron, Meurthe-et-Moselle, France.
Flying a Nieuport 28 C.1, he engaged by a Rumpler two-place observation plane of Reihenbildzug Nr. 3, a photographic reconniassance unit, flown by Gefreiter Kirschbaum and Leutnant Schieibe. Lufbery’s fighter was hit by gunfire from the Rumpler. The Deutsche Luftstreitkräfte airplane was later shot down and its crew captured.
Lufbery’s Nieuport rolled inverted, and he fell from the airplane. He was killed on impact.
Raoul Lufbery is considered to have been the first American “ace,” although all sixteen of his officially-credited aerial victories took place while in the service of France.
Major Gervais Raoul Victor Lufbery, 94th Aero Squadron, American Expeditionary Force, with a Nieuport 28 C.1 fighter, 1918.
Gervais Raoul Victor Lufbery was a dual American and French citizen, born 14 March 1885 at Chamalières, Puy-de-Dôme, France. He was the fourth child of Edward Lufbery, an American chemist, and Anne Joséphine Vessière Lufbery. Mme Lufbery died when he was about one year old. His father left Gervais in the care of his maternal grandmother, Madeline Vessière Greniere, and returned to the United States. Gervais grew up in France.
In 1907, at the age of 22, Lufbery traveled to America to visit family members in Connecticut. After traveling around the country and working in various occupations, Lufbery enlisted in the United States Army. He was assigned from the recruit depot Fort McDowell, Angel Island, San Francisco, to Company F, 20th Infantry Regiment, at the newly establish Fort Shafter, Territory of Hawaii, 13 December 1908. From 1 April 1909, Lufbery was stationed with Co. M, at the Presidio of Monterey in California. In 1910, he was sent to the Quartel de Espana, Manila, Philippine Islands.
After completing his term of service with the United States Army, in 1914 Lufbery enlisted in the Légion Étrangère (the French Foreign Legion). He was initially assigned as an aircraft mechanic, but was soon trained as a pilot. In 1916, Sergent Lufbery was assigned to a newly-formed unit, N-124,¹ Escadrille Lafayette of the Aéronautique Militaire (the French Air Service) which was made up primarily of volunteers from America. (The United States did not enter the War until 6 April 1917.)
Lufbery shot down his first enemy airplane 30 July 1916, and his fifth, 12 October 1916.
Sergent Lufbery was awarded the Médaille Militaire 11 September 1916. He was promoted to Adjutant, a non-commissioned officer rank. Adjutant Lufbery was awarded his first Croix de Guerre avec palme 26 September 1916, and his second, 28 October 1916. He was appointed a Chevalier de la légion d’honneur 10 March 1917. Lufbery was promoted to the commissioned rank of Sous lieutenant des Troupes Aeronautiques. Additional awards of the Croix de Guerre followed on 15 May, 15 June, 13 October, 29 October, 9 November 1917, and 11 January 1918.
Between 30 July 1916 and 2 December 1917, while serving with the Aéronautique Militaire, Lufbery shot down sixteen enemy airplanes (officially credited).
Sous-lieutenant Gervais Raoul Victor Lufbery, Aéronautique Militaire.
Sous lieutenant Lufbery was transferred to the 94th Aero Squadron, American Expeditionary Force, and was commissioned a major in the Aviation Section, Signal Officers’ Reserve Corps, United States Army.
Following his death, Major Lufbery was awarded the Purple Heart, and Britain’s Military Medal. His remains are interred at the Lafayette Memorial du Parc de Garches, Paris, France.
Nieuport 28 C.1 serial number 6215.
The Nieuport 28 C.1 ² was a single-place, single-engine, single-bay biplane fighter built by Société Anonyme des Éstablissements Nieuport for the French military. It was rejected, however, in favor of the SPAD S.XIII C.1. The new United States’ Air Service was in great need of fighters. There were none available of American manufacture, and because the new SPAD was in great demand, 297 Nieuport 28s were acquired by the American Expeditionary Force and assigned to the 94th and 95th Aero Squadrons.
The Nieuport 28 C.1 was 6.30 meters (20 feet, 8 inches) long with an upper wingspan of 8.160 meters (26 feet, 9¼ inches), lower wingspan of 7.79 meters ( 25 feet, 6-2/3 inches) and height of 2.30 meters (7 feet, 6½ inches). The upper wing had a chord of 1.30 meters (4 feet, 3.2 inches), and the lower, which was staggered behind the upper, had a chord of 1.00 meters (3 feet, 3.4). The upper wing had very slight dihedral, while the lower wing had none. Its empty weight was 399 kilograms (880 pounds) and loaded weight was 626 kilograms (1,380 pounds).
The Nieuport 28 C.1 was powered by an air-cooled, normally-aspirated 15.892 liter (969.786-cubic-inch-displacement) Gnome Monosoupape 9 Type N nine-cylinder rotary engine with a compression ratio of 5.45:1. The Monosoupape had a single overhead exhaust valve actuated by a pushrod and rocker arm. As the pistons reached the bottom of their exhaust strokes, a series of intake ports near the bottom of the cylinder were uncovered. The intake charge was drawn from the engine crankcase. The Type N produced 160 horsepower at 1,300 r.p.m. and turned a two-bladed fixed-pitch wooden propeller with a diameter of 2.50 meters (8 feet, 2.4 inches). The engine weighed 330 pounds (150 kilograms).
The Nieuport 28 had a top speed of 198 kilometers per hour (123 miles per hour) at 2,000 meters (6,562 feet) and 1,380 r.p.m., a range of 290 kilometers (180 miles) and a service ceiling of 5,300 meters (17,388 feet). Duration at full power was 1 hour, 45 minutes.
Two .303-caliber Vickers machine guns were mounted on the cowling, firing forward through the propeller arc.
Nieuport 28 C.1, serial number 6215.
¹ The “N” indicates that Escadrille 124 was equipped with Nieuport fighters. When the squadron transitioned to SPADs, the designation changed to SPA 124.
² “C.1” was the French designation for a single-place chasseur, their World War I term for what we now consider to be a fighter.
