The Curtiss-Wright XP-40 prototype, 36-10, at Langley Field in the original configuration. Compare this to the first production P-40 Warhawk in the photograph below. (NASA)Curtiss-Wright P-40 Warhawk 39-156. (U.S. Air Force)
24 April 1939: Curtiss-Wright’s prototype fighter, the XP-40 (Model 75P), was evaluated by the National Advisory Committee for Aeronautics (NACA) at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia, in March and April 1939. NACA engineers placed the XP-40 inside the Full-Scale Wind Tunnel, which was capable of accepting airplanes with wing spans of up to 40 feet (12.2 meters).
Compare this production Curtiss-Wright P-36A Hawk to the first production P-40 Warhawk in the photograph below.Curtiss Model 81, P-40 Warhawk, 39-156. (San Diego Air and Space Museum Archive)
The airplane was a production Curtiss P-36A Hawk, serial number 38-10, which had been modified by replacing its original air-cooled Pratt & Whitney Twin Wasp S1C1-G (R-1830-17) 14-cylinder radial engine with a Harold Caminez-designed, liquid-cooled, supercharged, 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Co. V-1710-C13 (V-1710-19).
This was a single overhead cam (SOHC) 60° V-12 engine with four valves per cylinder and a compression ration of 6.65:1. It had a Normal Power rating of 910 horsepower at 2,600 r.p.m. at Sea Level, and 1,060 horsepower at 2,950 r.p.m. for Takeoff. At 10,000 feet (3,048 meters), the V-1710-19 had Maximum Continuous Power rating of 1,000 horsepower at 2,600 r.p.m., and Military Power rating of 1,150 horsepower at 2,950 r.p.m. The engine required 100/130-octane aviation gasoline. It drove a three-bladed Curtiss Electric constant-speed propeller through a 2:1 gear reduction.
The V-1710-19 was 8 feet, 1.75 inches (2.483 meters) long, 3 feet, 4.75″ (1.035 meters) high and 2 feet, 4.94 inches (0.735 meters) wide. It weighed 1,320 pounds (599 kilograms).
Curtiss-Wright XP-40 prototype in the NACA wind tunnel at Langley Field, Virginia, 24 April 1939. The technician at the lower left of the photograph provides scale. (NASA)
The primary benefit of the engine change was the streamlined fuselage that resulted. The new airplane was capable of a speed of 366 miles per hour (589 kilometers per hour), a 53 miles per hour (85 kilometers per hour) increase over the P-36.
Over a two-month period, NACA engineers made a number of improvements. The radiator was moved forward under the engine and the oil coolers utilized the same air scoop. The exhaust manifolds were improved as were the landing gear doors.
When they had finished, Lieutenant Benjamin Scovill Kelsey flew the modified XP-40 back to Curtiss at Buffalo, New York. Its speed had been increased to 354 miles per hour (570 kilometers per hour), a 12% improvement. Other improvements were recommended which may have increased the XP-40’s speed by an additional 18 miles per hour (29 kilometers per hour). By December 1939, the airplane had been further improved and was capable of 366 miles per hour (589 kilometers per hour).
These photographs show the full-size prototype in the NACA wind tunnel at Langley, 24 April 1939. Two days later, the U.S. Army Air Corps ordered 524 airplanes as the P-40 Warhawk. By the time production ended in 1945, 13,738 Warhawks had been built.
Curtiss XP-40 in the NACA full scale wind tunnel, Langley Field, Virginia, April 1939. (NASA)
“Miss Elinor Smith, 17 years old, waving to the crowd of thousands, just after she landed here after establishing a new women’s flight endurance record, 26 hours, 21 minutes, 32 seconds, over four hours better than that of Mrs. McPhetridge of Los Angeles. The plucky girl flew a Ballanca cabin monoplane.” (George Rinhart/Corbis via Getty Images)Elinor Smith with the Bellanca (CTIE/Monash University)
24 April 1929: At Roosevelt Field, Mineola, Long Island, New York, 17-year-old Elinor Smith set a Fédération Aéronautique Internationale (FAI) World Record for Duration by staying aloft over Roosevelt Field, Long Island, New York, in a Bellanca CH Monoplane for 26 hours, 27 minutes. ¹ Miss Smith had very nearly doubled her own record, set just four months earlier. ²
During the flight the airplane’s elevator trim adjustment malfunctioned, forcing Smith to use both arms to hold the stick back to maintain level flight. She dropped a note in a weighted sack to advise those on the ground of the problem.
Elinor Smith with the Bellanca CH Monoplane. (Associated Press/The Los Angeles Times)
The Associated Press reported the event:
FLAPPER ‘ACE’ TOPS WOMEN’S AIR RECORDS
Elinor Smith Is Up Above 26 Hours; Victor Over Four.
By Associated Press,
ROOSEVELT FIELD, N.Y., April 24.—Elinor Smith, 17-year-old flying flapper of Long Island, won a victory Wednesday in the four-sided battle being waged among two women from the eastern seaboard and two from the west for the women’s solo endurance record.
She brought her plane down at 2:2:16 p.m. after 26 hours 21 minutes and 32 seconds in the air, beating the record of 22 hours 3 minutes and 12 seconds established by Louise McPhetridge of California by hours 18 minutes and 20 seconds.
Before Mrs. McPhetridge, Miss Bobbie Trout of California was the record holder. Miss Trout beat an earlier record of Miss Smith, who in turn on that earlier flight beat a record held by Viola Gentry, Long Island’s flying cashier.
Miss Smith’s record Wednesday was within 9 hours, 11 minutes and 49 seconds of the man’s solo endurance flight record of 35 hours, 33 minutes and 21 seconds, established at Roosevelt Field last month by Martin Jensen.
Beats Early Mark
Less than three minutes before, Miss Smith exceeded the first world endurance record ever established at this field. In 1921, Eddie Stinson of Detroit and Lloyd Bertaud, who was lost with the transatlantic plane Old Glory, established a record there of 26 hours, 18 minutes and 35 seconds, which was 2 minutes and 57 seconds less than the record set single-handed Wednesday by Miss Smith.
About 8:30 a.m. a note was dropped from the plane in which the young flier was having trouble with the stabilizer and had both arms “wrapped around the stick.”
Sure of Victory
It was apparent, however, that she did not regard the trouble as serious for the note added: “Tough night but it won’t be long now.”
Miss Smith brought her plane, a cabin monoplane borrowed from G.M. Bellanca, airplane designer, down to a perfect landing.
“I think it’s wonderful that I broke the record. Now I want to get some sleep,” she said as she dodged the crowds and vanished homeward.
Miss Smith’s mother Wednesday night said plans had been made for Elinor to make a transatlantic flight this summer, probably to Rome. She said backers already had been obtained.
—The Milwaukee Sentinel, April 25, 1929, Page 1, Column 4.
A Bellanca CH-200 (San Diego Air & Space Museum Archives)
The Bellanca CH Monoplane (also referred to as the CH-200) was a single-engine high-wing monoplane, designed by Giuseppe Mario Bellanca and built by the Bellanca Aircraft Corporation of America, Newcastle, Delaware. It was operated by one pilot and could carry up to 5 passengers in an enclosed cabin.
The airplane was 27 feet, 9 inches (8.458 meters) long with a wingspan of 46 feet, 4 inches (14.122 meters) and height of 8 feet, 4 inches (2.540 meters). It had an empty weight of 2,275 pounds (1,032 kilograms) and gross weight of 4,072 pounds (1,847 kilograms).
The Bellanca CH Monoplane was powered by an air-cooled, normally-aspirated 787.26-cubic-inch-displacement (12.901 liter) Wright Whirlwind J-5 nine-cylinder radial engine with a compression ratio of 5.1:1. It was rated at 200 horsepower at 1,800 r.p.m., and 225 horsepower at 2,000 r.p.m. This was a direct-drive engine which turned a two-bladed propeller. The Wright J-5C was 2 feet, 10 inches (0.864 meters) long and 3 feet, 9 inches (1.143 meters) in diameter. It weighed 508 pounds (230.4 kilograms).
The airplane’s maximum speed was 126 miles per hour (203 kilometers per hour) and its range was 800 miles (1,287 kilometers).
Elinor Regina Patricia Ward (Smith)
Elinor Regina Patricia Ward was born in New York City, 17 August 1911. She was the second of three children of Thomas Francis Ward, a vaudeville dancer and comedian, and Agnes A. Ward, a singer. In order to avoid being mistaken for another performer, Mr. Ward changed his name to Smith. Miss Ward also adopted the name and is better known as “Elinor Smith.”
Miss Smith took her first flight in an airplane at the age of six years. When she was ten she began flight training in her father’s Weaver Aircraft Co. Waco 9 biplane. Just before her seventeenth birthday she qualified for a pilot’s certificate. It was issued 14 August 1928 by the National Aeronautic Association of the U.S.A., on behalf of the Fédération Aéronautique Internationale. Certificate No. 6906 was signed by Orville Wright, Chairman of the N.A.A.
The National Aeronautic Association issued Aviator Pilot Certificate No. 6906 to Elinor Smith on 14 August 1928, just before her 17th birthday. The document was signed by Orville Wright.Elinor Smith flying under the Manhattan Bridge, 21 October 1928.
Elinor Smith first came to the attention of the general public when, on 21 October 1928, she flew under four bridges on New York City’s East River.
In November 1928 Miss Smith was employed by the Irvin Air Chute Company as a pilot. She toured the United States, flying a Bellanca Pacemaker.
On 10 March 1930, Smith set an FAI world altitude for women of 8,357 meters (27,418 feet). ³ She flew a Bellanca Skyrocket, NC752W.
In May 1930, the Aeronautics Branch, U.S. Department of Commerce issued a Transport License to Miss Smith. She was the youngest pilot to receive that license up to that time.
A 1930 poll of licensed pilots in the United States selected Smith as the Best Woman Pilot in America. Her male counterpart was the legendary Jimmy Doolittle.
Elinor Smith set several U.S. national records for speed, altitude and duration. From 1930 to 1935, she was an expert commentator on aviation for the National Broadcasting Company (NBC) radio network.
On 22 July 1933, Patrick H. Sullivan II, an attorney and member of the New York State Assembly for the 11th District of New York County, married Elinor Smith in New York City. They would have four children. Following the birth of their first child, Patrick H. Sullivan III, Mrs. Sullivan gave up flying.
Elinor Smith was featured on the box of Wheaties breakfast cereal in 1934. (General Mills)
In 1934, Mrs. Sullivan became the first woman to be featured on the box of General Mills’ Wheaties breakfast cereal, “The Breakfast of Champions.” This has always been a high honor for sporting men and women.
After her husband died in 1956, Elinor Smith Sullivan resumed flying, and continued until she was 89 years old.
Mrs. Elinor Smith Sullivan died 19 March 2010 at Lytton Gardens Health Care Center, Palo Alto, California. She was aged 98 years, 7 months and 3 days.
¹ FAI Record File Number 12217. Duration: 26 hours, 27 minutes. 24 April 1929.
² FAI Record File Number 12216. Duration: 13 hours, 17 minutes, 45 seconds. 31 January 1929.
³ FAI Record File Number 12226. Altitude, Female: 8,357 meters (27,418 feet), 10 March 1930.
Elinor Smith and a National Aeronautic Association official check a barograph following an altitude record attempt, 10 March 1930. (Smithsonian Institution, National Air and Space Museum)
North American Aviation Mustang Mk.I AG345, c/n 73-3098, prior to camouflage paint. Note the short carburetor air intake compared to the photograph of the camouflaged airplane, below. The RAF serial number, barely visible, is stenciled on the rudder just beneath the trim tab. (North American Aviation Inc. 73-0-6)
23 April 1941: At North American Aviation’s Inglewood, California factory, test pilot Louis Sanford Wait takes the very first production Mustang Mk.I, AG345, (c/n 73-3098) for its first flight.
The Royal Air Force had contracted with NAA to design and build a new fighter with a 1,200 horsepower Allison V-1710 supercharged 12-cylinder engine. The first order from the British Purchasing Commission was for 320 airplanes, and a second order for another 300 soon followed.
Mustang Mk.I AG345. (North American Aviation, Inc. 73-0-5)
The Mustang Mk.I (NAA Model NA-73) was a single-place, single-engine fighter primarily of metal construction with fabric control surfaces. It was 32 feet, 3 inches (9.830 meters) long with a wingspan of 37 feet, 5/16-inches (11.373 meters) and height of 12 feet, 2½ inches (3.721 meters). The airplane’s empty weight was 6,280 pounds (2,849 kilograms) and loaded weight was 8,400 pounds (3,810 kilograms).
North American Aviation Mustang Mk.I AG345 (North American Aviation Inc.)
The Mustang Mk.I was powered by a liquid-cooled, supercharged 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Company V-1710-F3R (V-1710-39) single overhead cam (SOHC) 60° V-12 engine with a compression ratio of 6.65:1. The -F3R had a Maximum Continuous Power rating of 880 horsepower at 2,600 r.p.m. at Sea level, and 1,000 horsepower at 11,000 feet (3,353 meters). It was rated at 1,150 horsepower at 3,000 r.p.m. for Take Off and Military Power. The Allison V-12 drove a 10 foot, 9 inch (3.277 meter) diameter, three-bladed Curtiss Electric constant-speed propeller through a 2.00:1 gear reduction. The V-1710-F3R was 7 feet, 4.38 inches (2.245 meters) long, 3 feet, 0.54 inches (0.928 meters) high, and 2 feet, 5.29 inches (0.734 meters) wide. It weighed 1,310 pounds (594 kilograms).
North American Aviation Mustang Mk.I AG345 (North American Aviation Inc.)
The Mustang Mk.I had a cruise speed of 311 miles per hour (500.5 kilometers per hour) at 75% power, and a maximum speed of 384 miles per hour (618 kilometers per hour) at 19,000 feet (5,791 meters). The airplane could reach 20,000 feet (6,096 meters) in 8.80 minutes. The service ceiling was 32,000 feet (9,754 meters) and its range was 640 miles (1,030 kilometers).
The Mk.I was equipped with four Browning AN-M2 .50-caliber machine guns, with one in each wing and two mounted in the nose under the engine. Four Browning .303 Mk.II machine guns were also installed, with two in each wing.
North American Aviation Mustang Mk.I AG345 (c/n 73-3098), front. (North American Aviation Inc.)
The Mk.I was 30 m.p.h. (48 kilometers per hour) faster than its contemporary, the Curtiss P-40 Warhawk, though both used the same engine. Below 15,000 feet (4,572 meters), the Mustang was also 30–35 m.p.h (48–56 kilometers per hour) faster than a Supermarine Spitfire, which had the more powerful Roll-Royce Merlin V-12.
Two Mustang Mk.Is were taken from the first RAF production order and sent to Wright Field for testing by the U.S. Army Air Force. These airplanes, assigned serial numbers 41-038 and 41-039, were designated XP-51. They would be developed into the legendary P-51 Mustang. In production from 1941 to 1945, a total of 16,766 Mustangs of all variants were built.
The first production Mustang Mk.I, AG345, first flight, 23 April 1941. (North American Aviation, Inc.)
Louis Sanford Wait was born 28 June 1908 at Superior, Nebraska. He was the first of two children of Dr. James Enos Wait, a dentist, and Alice Caroline Harrington Wait.
Wait enlisted in the Air Corps, United States Army, as an aviation cadet, in 1929. He trained as a pilot at March Field, near Riverside, California, and at Kelly Field, Bexar, Texas. Wait graduated 27 June 1930 and received his pilot’s wings and a commission as a second lieutenant, Air Corps Reserve. (O274973) Lieutenant Wait trained as an attack pilot and was assigned to Fort Crockett, Galveston, Texas.
From 1932 to 1935, Wait, having been released from active duty, was employed as a test pilot for the Boeing Airplane Company, Seattle, Washington.
By 1937, Lieutenant Wait was assigned to Headquarters Squadron, 2nd Bombardment Group at Langley Field, Virginia, under the command of Brigadier General Robert Olds. While on 18 days leave, on 3 December 1937, Second Lieutenant Wait married Mrs. Elsie O. Callow (née Elsie Oliver) at Amityville, New York.
Wait married Mrs. Mary Elizabeth Croxen (née Mary Elizabeth Musser), 2 November 1944, in Los Angeles, California.
In August 1946, Louis Wait entered a P-51C Mustang, NX28388, in the Bendix Trophy Race. The airplane had been purchased by Jackie Cochran. She flew it in the race and finished in second place behind Paul Mantz.
In 1951, Wait was appointed general administrator of a new North American Aviation plant at the Fresno Air Terminal, Fresno, California. The plant, which employed about 400 people, manufactured and repaired parts for the T-6/SNJ Texan flight trainers, and performed modifications to F-86 Sabre jet fighters.
Louis Sanford Wait died 3 July 1963, at the age of 55 years.
1st Lieutenant Paul Frank Baer, Air Service, United States Army. (Campbell Studios, New York)
23 April 1918: at 09:55 a.m., near Saint-Gobain, France, 1st Lieutenant Paul Frank Baer, 103rd Aero Squadron (Pursuit), shot down an enemy Albatross C two-place biplane. This was Baer’s fifth victory in aerial combat, making him the first American “ace.” ¹ [Official credit for this shoot-down is shared with Lt. C. H. Wilcox.]
Albatros C.VII C.2197/16 (Wikipedia)
Paul Frank Baer was born 29 January 1894 at Fort Wayne, Indiana, the fourth of four children of Alvin E. Baer, a railroad engineer, and Emma B. Parent Baer.
In 1916, Baer served under Brigadier John J. General Pershing during the Mexican Expedition to capture the outlaw and revolutionary Francisco (“Pancho”) Villa. He then went to France and enlisted the Aéronautique Militaire, in 20 February 1917. He was sent for flight training at the Avord Groupemant des Divisions d’Entrainment (G.D.E.). He graduated as a pilot, 15 June 1917, with the rank of corporal.
After flight training, Corporal Baer was assigned to Escadrille SPA 80, under the command of Capitaine Paul Ferrand, 14 August 1917 to 20 January 1918, flying the SPAD S.VII C.1 and SPAD S.XIII C.1. Baer was next transferred to Escadrille N. 124, the EscadrilleAméricaine, under Georges Thénault. This unit was equipped with the Nieuport-Delâge Ni-D 29 C1.
Nieuport-Delâge Ni-D 29C.1, s/n 12002, right front quarter view.
After the United States entered the War, Baer was transferred to the 103rd Aero Squadron, American Expeditionary Forces, and commissioned as a 1st Lieutenant with a date of rank retroactive to 5 November 1917. At that time, the 103rd was under the command of Major William Thaw II, and was operating near La Cheppe, France, flying the SPAD S.VII C.1 chasseur.
SPAD S.XIII C.1 S7714 of the 103rd Aero Squadron, France, 1918. The pilot is Captain Robert Soubiran, the squadron’s commanding officer. (U.S. Air Force)
Lieutenant Baer is officially credited by the United States Air Force with 7.75 enemy airplanes shot down between 11 March and 22 May 1918, ² and he claimed an additional 7. (Credit for two airplanes was shared with four other pilots.) After shooting down his eighth enemy airplane on 22 May 1918, Baer and his SPAD S.XIII C.1 were also shot down. He was seriously injured and was captured by the enemy near Armentières and held as a Prisoner of War. At one point, Baer was able to escape for several days before being recaptured.
For his service in World War I, 1st Lieutenant Paul Frank Baer was awarded the United States’ Distinguished Service Cross with one oak leaf cluster (a second award). He was appointed Chevalier de laLégion d’honneur by Raymond Poincaré, the President of France. He was also awarded the Croix de Guerre with seven palms.
SPAD S.XIII C.1 at Air Service Production Center No. 2, Romorantin Aerodrome, France, 1918. (U.S. Air Force)
After World War I, Baer, as a “soldier of fortune,” organized a group of pilots to fight against “the Bolsheviks” in Poland. He returned to the United States, departing Boulogne-sur-mer aboard T.S.S. Nieuw Amsterdam, and arriving at New York City, 4 November 1919. He then flew as a test pilot, an air mail pilot in South America, and worked as an aeronautical inspector for the U.S. Department of Commerce, based at Brownsville Airport, Texas. In 1930, he was employed as a pilot for the China National Aviation Corporation.
Baer was flying from Nanking to Shanghai for with an amphibious Loening Air Yacht biplane, named Shanghai. The airplane crashed after striking the mast of a boat on the Huanpu River. He died at the Red Cross Hospital at Shanghai, China, at 9:00 a.m., 9 December 1930. A Chinese pilot, K. F. Pan, and an unidentified female passenger were also killed. General Hsiung Shih-hui and four other passengers on board were seriously injured.
Paul Baer’s remains were returned to the United States aboard S.S. President McKinley and were buried at the Lindenwood Cemetery in Fort Wayne, Indiana.
In 1925 a new airport was opened in Fort Wayne and named Paul Baer Municipal Airport. During World War II, the airport was taken over by the military and designated Baer Army Airfield. It is now Fort Wayne International Airport (FWA).
A CNAC Loening Air Yacht amphipian at Lungwha, China, circa 1930. (SFO Aviation Museum & Library R2014.1811.001)Lufbery
¹ TDiA would like to thank CMSgt Bob Laymon USAF (Ret.) (AKA, “Scatback Scribe”) for pointing out that while Lt. Baer was the first American to become an ace flying in the American service, that,
² U.S. AIR SERVICE VICTORY CREDITS, WORLD WAR I, USAF Historical Study No. 133, Historical Research Division, Air University, Maxwell Air Force Base, Alabama, June 1969, at Page 7
Lieutenant Commander Patrick Neison Lynch Bellinger, United States Navy.
23 April 1915: Lieutenant Patrick Neison Lynch Bellinger, United States Navy, flew a Burgess-Dunne hydroaeroplane to an altitude of 10,000 feet (3,048 meters) over Pensacola Bay, Florida.
The Aero Club of America certified Lieutenant Bellinger’s record:
Homolgation of the altitude record made by Lieut. P. N. L. Bellinger at Pensacola Bay, Fla., on April 23rd last has been officially recognized and awarded as follows: American altitude record, aviator alone, hydroaeroplane, 10,000 feet. This height was reached in one hour, nineteen minutes. It is interesting to note the climbing record in connection with this flight, 6,000 feet being attained in 24 minutes and 8,000 feet in 41 minutes.
—Flying, Vol. IV, No. 5, June, 1915, The Aero Club of America, Club News, Page 554 at Column 1
Burgess-Dunne hydroaeroplane, U.S.N. serial number AH-10. (United States Navy)Lieutenant John William Dunne, Wiltshire Regiment, British Army. (The Sketch, 19 May 1909)
The Burgess-Dunne Model BD-5, U.S. Navy serial number AH-10, was a licensed variant of the British Short Brothers-built Dunne D.5. The configuration was designed by Lieutenant John William Dunne, F.R.Ae.S., and was based on his observations of the Roemer’s Alsomitra macrocarpa seeds, although his design essentially reversed the aerodynamic features of the seed.
According to Wikipedia:
The seed or samara of this species is unusual in having two flat bracts extending either side of the seed to form a wing-like shape with the seed embedded along one long edge and the wings angled slightly back from it. As the seed ripens the wings dry and the long edge furthest from the seed curls slightly upwards. When ripe, the seed drops off and its aerodynamic form allows it to glide away from the tree.[6][7] The wing spans some 13 cm and can glide for great distances. The seed moves through the air like a butterfly in flight — it gains height, stalls, dips and accelerates, once again producing lift, a process termed phugoid oscillation.[8] In the past it was often found on the decks of ships at sea.
The seed’s relative stability in pitch and roll inspired Igo Etrich, a pioneer of early aviation. The contemporary pioneer J.W. Dunne also studied the seed but discarded it as inspiration because it was not directionally stable.
Alsomitra macrocarpa seed. (Scott Zona/Wikipedia)
The BD-5 was a two-place, single-engine, four-bay biplane with a single pontoon and wingtip-mounted floats. The wings were swept 30° and the lower wing was staggered significantly behind the upper. Both wings had anhedral, and the upper wing had slightly more area and a negative twist. There was no tail, rudder or elevators. The ailerons also acted as elevators. The design was very stable and it could not be forced into a stall.
Burgess-Dunne Hydroaeroplane, 1914. (FLIGHT First Aero Weekly in the World, No. 286 (Vol. VI, No. 25), 19 June 1914 at page 645.)
The Burgess-Dunne was 24 feet, 8 inches (7.518 meters) long, with a wingspan of 46 feet, 0 inches (14.021 meters). The wings have a chord of 6 feet, 0 inches (1.829 meters) vertical gap between the wings was 6 feet, 0 inches (1.829 meters). The total wing area is 545 square feet (50.63 square meters). The airplane’s empty weight was 1,450 pounds (658 kilograms), and it had a gross weight of 1,700 pounds (771 kilograms).
The pontoon had a single hydrodynamic step. It was 17 feet, 8 inches (5.385 meters) long, 3 feet, 1 inch (0.940 meters) wide and had a maximum depth of 1 foot, 2 inches (0.356 meters).
The airplane was powered by a water-cooled, normally-aspirated 567.450-cubic-inch-displacement (9.299 liter) Curtiss OXX-2 overhead valve 90° V-8 engine with dual ignition. It had two valves per cylinder, a compression ratio of 4.92:1, and produced 100 horsepower at 1,400 r.p.m. The OXX-2 was a direct-drive engine and turned a two-bladed, 8 foot (2.4 meter) diameter propeller in a pusher configuration.
The Burgess-Dunne had a fuel capacity of 22 Imperial gallons (100 liters) and carried 4 gallons (18 liters) of lubricating oil.
During flight testing, the Burgess-Dunne Hydroaeroplane averaged 58.75 miles per hour (94.55 kilometers per hour) ground speed over a triangular course with a 10 knot wind (11.5 miles per hour, or 5.4 meters per second).
One Burgess-Dunne had been ordered by the Navy on 5 December 1914. The cost was $5,000.00, less engine. It was delivered in April, 1915. After being flown to the altitude record, AH-10 was used for artillery spotting at Fort Monroe, Virginia. It was the first U.S. Navy aircraft to be armed with a machine gun, a .30-caliber Benét-Mercié machine rifle, and bomb racks.
On 7 March 1916, AH-10 was damaged in a collision with a sailing vessel off Mobile, Alabama. The pilot, Lieutenant Edward Orrick McDonnell, U.S. Navy, was not hurt. After repair, the airplane was returned to service. (Lieutenant McDonnell had been awarded the Medal of Honor for his actions at the Battle of Veracruz, 21–22 April 1914. He rose to the rank of Vice Admiral.)
Burgess-Dunne AH-10 hydroaeroplane at Naval Air Station Pensacola, Florida, circa 1917. (National Naval Aviation Museum)
Patrick Neison Lynch Bellinger was born 8 October 1885 at Cheraw, South Carolina. He was the son of Carnot Ambrose Bellinger and Eleanor Lynch Bellinger.
A 1907 graduate of the U.S. Naval Academy, Annapolis, Maryland, he served at sea aboard the battleship USS South Carolina (BB-26) before being assigned as commanding officer of the C-class submarine, C-4 (SS-15). He was then trained as an airplane pilot. Lieutenant Bellinger was Naval Air Pilot No. 4.
United States Navy Submarine C-4, circa 1912–1914. (U.S. Navy NH92096)
During the Veracruz campaign, 1914, Lieutenant Bellinger flew reconnaissance over enemy lines. It was here that a United States military airplane first came under enemy fire. He was nominated for the Medal of Honor for his actions there.
Lieutenant Commander Bellinger, United States Navy, circa 1919.
In 1919 he was awarded the Navy Cross, “For distinguished service in the line of his profession as commanding officer of the seaplane NC-1 which made a long overseas flight from Newfoundland to the vicinity of the Azores in May 1919.”
Lieutenant Commander Bellinger married Elsie McKeown of Pennsylvania, 24 July 1915. She died at Washington, D.C., 9 February 1920. He married his second wife, Miriam Georgia Benoist, 14 April 1921.
Bellinger progressively rose in rank and responsibility. As rear admiral, he commanded Patrol Wing 2 at Pearl Harbor at the time of the surprise attack by the Imperial Japanese Navy. During World War II, he was promoted to the rank of Vice Admiral and served as Commander Air Force, Atlantic Fleet. Vice Admiral Bellinger retired from the Navy in 1947.
Vice Admiral Patrick Neison Lynch Bellinger, United States Navy (Retired), died 29 May 1962 at the Chesapeake & Ohio Hospital, Clifton Forge, Virginia. He is buried at the Arlington National Cemetery.
Lieutenant Commander Patrick N. L. Bellinger, U.S. Navy. (Portrait by Harris & Ewing, Washington D.C., 18 January 1920)
24 April 1939: Curtiss-Wright’s prototype fighter, the XP-40 (Model 75P), was evaluated by the National Advisory Committee for Aeronautics (NACA) at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia, in March and April 1939. NACA engineers placed the XP-40 inside the Full-Scale Wind Tunnel, which was capable of accepting airplanes with wing spans of up to 40 feet (12.2 meters).
