Tag Archives: James H. Doolittle

2 April 1942

B-25 Mitchell bombers aboard USS Hornet (CV-8), with USS Gwin (DD-433) and USS Nashville (CL-43), somewhere in the Pacific, April 1942. (U.S. Navy)
B-25 Mitchell bombers aboard USS Hornet (CV-8), with USS Gwin (DD-433) and USS Nashville (CL-43), somewhere in the Pacific, April 1942. (U.S. Navy)

2 April 1942: After loading sixteen North American Aviation B-25B Mitchell medium bombers and their crews of the 17th Bombardment Group (Medium) at NAS Alameda, the recently commissioned United States Navy aircraft carrier USS Hornet (CV-8) departed San Francisco Bay with her escorts and headed for a secret rendezvous with Vice Admiral William F. Halsey, Jr., and Task Force 16.

The new carrier was under command of Captain Marc A. Mitscher. The strike group was commanded by Lieutenant Colonel James H. (“Jimmy”) Doolittle, U.S. Army Air Corps. Until the second day at sea, only six U.S. military officers knew of the mission.

The photograph above shows some of the bombers secured on Hornet‘s flight deck. An escorting destroyer, USS Gwin (DD-433) is closing from astern, with light cruiser USS Nashville (CL-43) in the distance. Two more ships are on the horizon.

USS Hornet (CV-8), 27 October 1942. (U.S. Navy)
USS Hornet (CV-8), Captain Marc A. Mitscher, U.S.N., commanding, 27 October 1942. The aircraft carrier is painted in Measure 12 camouflage, Sea Blue 5-S, Ocean Gray 5-O and Haze Gray 5-H. (U.S. Navy)

USS Hornet was a brand new Yorktown-class aircraft carrier, commissioned 20 October 1941. It had just completed its shakedown cruise in the Atlantic when it was sent west for this mission.

The ship was 824 feet, 9 inches (251.384 meters) long, overall, with a maximum width of 114 feet (34.747 meters). Hornet‘s dimensions at the waterline (full load displacement) were 761 feet (232 meters) long with a beam of 83 feet, 3 inches (25.375 meters). Its draft was 28 feet (8.5 meters).

The flight deck had two hydraulic catapults, and three elevators for bringing aircraft up from the hangar deck. A third catapult was on the hangar deck, launching aircraft laterally.

Powered by four geared steam turbines driving four propeller shafts, Hornet‘s engines produced 120,000 shaft horsepower. The carrier’s maximum speed was 33.84 knots (39.94 miles per hour/62.67 kilometers per hour), and maximum range, 12,500 nautical miles (14,385 kilometers).

North American Aviation B-25B Mitchell medium bomber tied down on the flight deck of U.S.S. Hornet (CV-8). An escorting destroyer, USS Gwin, (DD- ) closes on the carrier's right rear quarter. (U.S. Navy)
A 17th Bombardment Group North American Aviation B-25B Mitchell medium bomber tied down on the flight deck of U.S.S. Hornet (CV-8). An escorting destroyer, USS Gwin, (DD-433 ), Commander John S. Higgins, U.S.N., commanding, closes on the carrier’s right rear quarter. The sixteen Army bombers used all the space available on Hornet’s flight deck.(U.S. Navy)

The aircraft carrier’s primary armament was its air wing, consisting of a squadron each of Grumman F4F Wildcat fighters, Douglas SBD Dauntless dive bombers and Douglas TBD Devastator torpedo bombers. For the Halsey-Doolittle Raid, Hornet‘s air wing was stored on the hangar deck and unavailable.

“To make room for the Army bombers, Hornet had struck her own planes below. Wildcats and Devastators, with wings folded, and dismantled SBDs were packed into every available space, even hung from the overhead. So, except for her few guns, the carrier was defenseless until she rendezvoused with Task Force 16. . . .”

History of United States Naval Operations in World War II, Volume III, The Rising Sun in the Pacific, by Samuel Eliot Morison, Little, Brown & Company, Boston, 1988, Chapter XX at Page 392.

For defense, the ship was lightly armored, with 2.5–4 inches (6.35–10.2 centimeters) of belt and deck armor. She also carried eight 5-inch, 38-caliber (5″/38) dual-purpose guns in single mounts, thirty 20mm Oerlikon autocannon, twenty water-cooled 1.1-inch, 75-caliber (1.1″/75) guns in four-gun mounts, and twenty-four Browning .50-caliber (12.7 millimeter) machine guns.

Including the ship’s air wing, the complement was 2,919 men.

USS Hornet fought at the Battle of Midway, June 3–7, 1942. She was sunk at the Battle of the Santa Cruz Islands, 26 October 1942, having been hit by two airplanes, 8 bombs, 16 torpedoes and an unknown number of 5-inch shells.¹

USS Hornet (CV-8) at Peral Harbor, Hawaii, following the Halsey-Doolittle Raid, 1942. The ships is painted in Measure 12 (Modified) camouflage, with Sea Blue 5-s, Ocean Gray 5-O and Haze Gray 5-H coloration.
USS Hornet (CV-8) at Pearl Harbor, Hawaii, following the Halsey-Doolittle Raid, 1942. The ship is painted in Measure 12 (Modified) camouflage with splotches, with Navy Blue 5-N, Sea Blue 5-S, Ocean Gray 5-O and Haze Gray 5-H coloration.

¹ The research vessel R/V Petrel located the wreck of USS Hornet on the sea floor in January 2019. The ship lies at a depth of 5,330 meters (17,487 feet).

© 2019, Bryan R. Swopes

26 October 1925

Lieutenant James H. Doolittle, USAAS, with the Curtiss R3C-2 Schneider Trophy winner, 1925. (U.S. Air Force)
Lieutenant James H. Doolittle, Air Service, United States Army, with the Curtiss R3C-2 Schneider Trophy winner, 1925. (U.S. Air Force)

26 October 1925: Lieutenant James Harold Doolittle, Air Service, United States Army, won the Coupe d’Aviation Maritime Jacques Schneider (commonly called the Schneider Trophy) when he placed first flying his Curtiss R3C-2 float plane over a 217-mile (349 kilometer) course near Bay Shores on Chesapeake Bay, Maryland.

Doolittle’s average speed for the seven laps around the triangular race course was 232.57 miles per hour (374.29 kilometers per hour). The second-place airplane, a Gloster-Napier III flown by Captain Hubert Broad, averaged 199.16 miles per hour (320.52 kilometers per hour).

Doolittle also set two Fédération Aéronautique Internationale (FAI) world records during the race: World Record for Speed Over 100 Kilometers, with an average speed of 377.83 kilometers per hour (234.77 miles per hour);¹  World Record for Speed Over 200 Kilometers, 377.16 kilometers per hour (234.36 miles per hour).²  On the following day, Doolittle set a third FAI record: World Record for Speed Over a 3 Kilometer Course, 395.5 kilometers per hour (245.75 miles per hour).³

Lt. Jmes H. Doolittle and Lt. Cyrus Bettis with the Curtiss R3C (NARA 31758AC)
Lieutenant James H. Doolittle (left) and Lieutenant Cyrus Bettis with the Curtiss R3C-2. (NARA 31758AC)

A contemporary news article commented on Jimmy Doolittle’s performance:

Gloster III Schneider Cup racer, powered by a 700 horsepower Napier Lion VII “broad arrow” W-12.

“. . . according to reports Lieut. Doolittle’s cornering was superb, and must have been to a great extent responsible for the excellent performance. Reports from America—coming, it is thought, from a reliable source—indicate that one particular engine out of the 12 built for the Pulitzer and Schneider Trophy races proved exceptionally good, as will often happen in a batch of engines, and it is believed that this engine was fitted in Doolittle’s Curtiss-Army Racer. This fact, taken in conjunction with the masterly handling of the machine, would seem to account for the wholly unexpected average speed maintained, which was, of course, far and away ahead of the speeds of the British and Italian competitors.”

FLIGHT, The Aircraft Engineer & Airships, No. 879 (No. 44, Vol. XVII.) October 29, 1923 at Page 703

“The triangular Schneider race course stretched from Bay Shore Park to Gibson Island to the south and across Chesapeake Bay to Huntingfield Point. Contestants had to fly the 50-kilometer (31-mile) course seven times.” Smithsonian National Air and Space Museum
The Curtiss R3C-2 Racer on display at the National Air and Space Museum. (Photo by Eric Long, National Air and Space Museum, Smithsonian Institution)
The Curtiss R3C-2 Racer on display at the National Air and Space Museum. (Photo by Eric Long, National Air and Space Museum, Smithsonian Institution)

The R3C-2 was a single-engine, single-seat, single-bay biplane, equipped with pontoons for taking off and landing on water. It was built especially for air racing. Two R3Cs were built for the United States Navy and one for the Army. (The Army aircraft is identified by a Navy Bureau of Aeronautics serial number (“Bu. No.”) A-7054. It does not seem to have been assigned an Air Service serial number.) The airplane and its V-1400 engine were both built by the Curtiss Aeroplane and Motor Company, which had been founded by Glenn Hammond Curtiss. The R3C-2 was converted from the R3C-1, the land plane configuration which had been flown by Lieutenant Cyrus Bettis, AS, USA, to win the Pulitzer Trophy Race just two weeks earlier.

The RC3-2 is 22 feet long (6.706 meters), an increase of 2 feet, 3.5 inches (0.698 meters) over the R3C-1 configuration, resulting from the replacement of the fixed wheeled landing gear with the single-step pontoons. The upper wing span is 22 feet (6.706 meters), with a chord of 4 feet, 8¼ inches (1.429 meters). The lower wing span is 20 feet (6.096 meters) with a chord of 3 feet, 3¾ inches (1.010 meters).  Weight empty was 2,135 pounds (968 kilograms) and maximum takeoff weight was 2,738 pounds (1,242 kilograms).

Constructed of wood, the fuselage has four ash longerons and seven birch vertical bulkheads. The framework is covered with two layers of 2-inch (51 millimeter) wide, 3/32-inch (2.38 millimeter) thick spruce strips. These were placed on a 45° diagonal from the fuselage horizontal centerline, with the second layer at 90° to the first. These veneer strips were glued and tacked to the frame. The fuselage was then covered with doped fabric. The wings and tail surfaces are also of wood, with spruce ribs and a covering of spruce strips.

Lieutenant Cyrus Bettis, USAAS, with the Curtiss R3C-1 racer at Mitchel Field, Long Island, New York, 12 October 1925. The surface radiators on the wings can be seen. (Curtiss Aeroplane and Motor Co.)

The single-bay wings are wire braced and contain surface radiators made of thin brass sheeting. The radiators contained 12 gallons (45.4 liters) of water, circulating at a rate of 75 gallons (283.9 liters) per minute. By using surface radiators to cool the engine, aerodynamic drag was reduced.

The Curtiss V-1400 engine was developed from the earlier Curtiss D-12. It was a water-cooled, normally aspirated, 1,399.91-cubic-inch-displacement (22.940 liter), dual overhead cam (DOHC) 60° V-12, with a compression ratio of 5.5:1. The V-1400 was rated at 510 horsepower at 2,100 r.p.m., and could produce 619 horsepower at 2,500 r.p.m. It was a direct-drive engine and turned a two-bladed duralumin fixed-pitch propeller with a diameter of 7 feet, 8 inches (2.337 meters). The propeller was designed by Sylvanus Albert Reed, Ph.D. The V-1400 engine weighed 660 pounds (299 kilograms).

The R3C-2 had a fuel capacity of 27 gallons (102 liters). Its range was 290 miles (467 kilometers).

The Coupe d’Aviation Maritime Jacques Schneider at the Science Museum, London. (Wikipedia, edit by Eric Menneteau)

Jimmy Doolittle was one of America’s foremost pioneering aviators. He set many records, won air races, tested and developed new flying equipment and techniques.

He was a highly-educated military officer, having earned his Bachelor of Arts from the University of California Berkeley School of Mines, and M.S and D.Sc. degrees in Aeronautical Engineering from the Massachusetts Institute of Technology.

During World War II, Colonel Doolittle planned and led the famous Halsey-Doolittle Raid against Japan, 18 April 1942, for which he was awarded the Medal of Honor.

As a brigadier general, he commanded 12th Air Force in North Africa. Promoted to major general, he was given command of the 15th Air Force in the Mediterranean Theater, and commanded 8th Air Force as a lieutenant general, 1943–1945.

After the war, Lieutenant General Doolittle was placed on the inactive list. On 4 April 1985, by Act of Congress, James H. Doolittle was promoted to General. General Doolittle is the only person to have been awarded both the Congressional Medal of Honor and the Presidential Medal of Freedom.

Jimmy Doolittle
First Lieutenant James Harold Doolittle, Air Service, United States Army

¹ FAI Record File Number 11866

² FAI Record File Number 11867

³ FAI Record File Number 11868

© 2018, Bryan R. Swopes

12 October 1925

Lieutenant Cyrus Bettis and his Curtiss R3C-1 cross the finish line at the 1925 Pulitzer Trophy Race. (NASM)
The Pulitzer Trophy

12 October 1925: At Mitchel Field, Long Island, New York, Lieutenant Cyrus Bettis, Air Service, United States Army, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over 100 kilometers (62.14 miles), flying a Curtiss R3C-1 racing plane, #43. His average speed was 401.28 kilometers per hour (249.34 miles per hour).¹ Lieutenant Bettis was awarded the Pulitzer Trophy.

Bettis also won the Mackay Trophy for 1925.

Cyrus Bettis had previously won the 1924 Mitchell Trophy Race, sponsored by Brigadier General Billy Mitchell in honor of his brother, John L. Mitchell, who was killed during World War I.

Lieutenant Cyrus Bettis, USAAS, with the Curtiss R3C-1 racer at Mitchel Field, Long Island, New York, 12 October 1925. The surface radiators on the wings can be seen. (Curtiss Aeroplane and Motor Co.)
Lieutenant Cyrus Bettis, USAAS, with the Curtiss R3C-1 racer at Mitchel Field, Long Island, New York, 12 October 1925. The surface radiators on the wings can be seen. (Curtiss Aeroplane and Motor Co.)

The Curtiss R3C-1 was a single-place, single-engine, single-bay  biplane built for especially for air racing.  Two were built for the United States Navy and one for the Army. (The Army aircraft is identified by a Navy Bureau of Aeronautics serial number (“Bu. No.”) A-7054. It does not seem to have been assigned an Air Service serial number.) The airplane and its V-1400 engine were built by the Curtiss Aeroplane and Motor Company, which had been founded by Glenn Hammond Curtiss. It was converted to a seaplane configuration with two single-step pontoons, the R3C-2, for the Schneider Trophy Race, two weeks later, 25 October.

The R3C is 19 feet, 8½ inches (6.007 meters) long. The upper wing span is 22 feet (6.706 meters), with a chord of 4 feet, 8¼ inches (1.429 meters). The lower wing span is 20 feet (6.096 meters) with a chord of 3 feet, 3¾ inches (1.010 meters). The R3C-1 had an empty of 2,135 pounds (968 kilograms) and its maximum takeoff weight was 2,738 pounds (1,242 kilograms).

Curtiss R3C-1 (FAI)
Lieutenant Bettis’ record-setting Curtiss R3C-1 biplane. (FAI)

Constructed of wood, the fuselage had four ash longerons and seven birch vertical bulkheads. The framework was covered with two layers of 2-inch (51 millimeter) wide, 3/32-inch (2.38 millimeter) thick spruce strips. These were placed on a 45° diagonal from the fuselage horizontal centerline, with the second layer at 90° to the first. These veneer strips were glued and tacked to the frame. The fuselage was then covered with doped fabric. The wings and tail surfaces were also of wood, with spruce ribs and a covering of spruce strips.

The single-bay wings were wire braced and contained surface radiators made of thin brass sheeting. The radiators contained 12 gallons (45.4 liters) of water, circulating at a rate of 75 gallons (283.9 liters) per minute. By using surface radiators to cool the engine, aerodynamic drag was reduced.

The Curtiss V-1400 engine was developed from the earlier Curtiss D-12. It was a water-cooled, normally aspirated, 1,399.91-cubic-inch-displacement (22.940 liter), dual overhead cam (DOHC) 60° V-12, with a compression ratio of 5.5:1. The V-1400 was rated at 510 horsepower at 2,100 r.p.m., and could produce 619 horsepower at 2,500 r.p.m. It was a direct-drive engine and turned a two-bladed duralumin fixed-pitch propeller with a diameter of 7 feet, 8 inches (2.337 meters). The propeller was designed by Sylvanus Albert Reed, Ph.D. The V-1400 engine weighed 660 pounds (299 kilograms).

The R3C-1 had a fuel capacity of 27 gallons (102 liters). Its range was 290 miles (467 kilometers).

After the Pullitzer race, the R3C-1 was reconfigured as a seaplane for the Schneider Trophy Race. The fixed landing gear was replaced by two single-step pontoons and the airplane was redesignated R3C-2. Additional fuel was carried in the pontoons. On 26 October 1925, 1st Lieutenant James H. Doolittle flew the airplane to win the Coupe d’Aviation Maritime Jacques Schneider at Chesapeake Bay, Maryland.

The R3C-2 is in the collection of the Smithsonian Institution National Air and Space Museum.

Lt. James H. Doolittle and Lt. Cyrus Bettis with the Curtiss R3C-2 (NARA 31758AC)
Lt. James H. Doolittle (left) and Lt. Cyrus Bettis with the Curtiss R3C-2 (NARA 31758AC)

Cyrus Bettis was born 2 January 1893, at Carsonville, Michigan, the first of three children of John Bettis, a farm worker, and Mattie McCrory Bettis.

Bettis enlisted as a private, first class, in the Aviation Section, Signal Enlisted Reserve Corps, at Detroit, Michigan, 23 January 1918. The Bell Telephone News reported:

     Cyrus Bettis has gone to Detroit and enlisted in the Aviation Corps of Uncle Sam’s service.

     He expects to be called to service at any time and will probably go East for training. Cyrus has been the efficient and genial manager of the Michigan State Telephone exchange in Fenton for several years. He has made an excellent manager and entrenched himself in the good graces of his patrons and Fenton People in General. —Fenton Independent.

Bell Telephone News, Volume 7, Number 6, January 1918, at Page 4, Column 1

On 11 September 1918, Cyrus Bettis was commissioned as a second lieutenant, Air Service, United States Army. This commission was vacated 16 September 1920 and he was appointed a second lieutenant, Air Service, with date of rank to 1 July 1920. On 21 March 1921, Bettis was advanced to the rank of first lieutenant, retroactive to 1 July 1920.

On 23 August 1926, flying from Philadelphia to Selfridge Field in Michigan, Bettis flew into terrain in fog in the Allegheny Mountains of western Pennsylvania. With a fractured skull and broken left leg, Bettis crawled several miles to a roadway where he was found, 43 hours after the crash.

Bettis was taken by air ambulance to Walter Reed Army Hospital, but died of spinal meningitis resulting from his injuries, 1 September. He was buried at the Lakeside Cemetery, Port Huron, Michigan.

1st Lieutenant Cyrus Bettis, Air Service, United States Army. (FAI)

¹ FAI Record File Number 9684

© 2017, Bryan R. Swopes

4 September 1922

Jimmy Doolittle with his DH-4 during a refueling stop at Kelly Field, San Antonio, Texas, 4 September 1922. (National Air and Space Museum Archives, Smithsonian Institution)
Jimmy Doolittle with his DH-4B-1-S, A.S. 22-353, during a refueling stop at Kelly Field, San Antonio, Texas, 4 September 1922. Photograph by H.L. Summerville. (National Air and Space Museum Archives, Smithsonian Institution)

4 September 1922: First Lieutenant James H. (“Jimmy”) Doolittle, Air Service, United States Army, made the first transcontinental crossing of the United States in a single day when he flew a DH.4B-1-S single-engine biplane, Air Service Serial Number 22-353, from Pablo Beach, Florida, ¹ to Rockwell Field, San Diego, California, a distance of 2,106 miles (3,390 kilometers). He made one refueling stop at Kelly Field, San Antonio, Texas, which lasted 1 hour, 16 minutes. The total duration of the flight was 21 hours, 19 minutes.

Lieutenant James H. Doolittle, in the cockpit of the DH-4B, is greeted on his arrival at Kelly Field, San Antonio, Texas. (Peter M. Bowers Collection)
Lieutenant James H. Doolittle, in the cockpit of the DH-4B, is greeted on his arrival at Kelly Field, San Antonio, Texas. (Peter M. Bowers Collection)

Lieutenant Doolittle was awarded the Distinguished Flying Cross for “demonstrating the possibility of moving Air Corps units to any portion of the United States in less than 24 hours.”

Maintenance technicians service Lieutenant Doolittle's DH-4B-S-1 at Kelly Field.
Maintenance technicians service Lieutenant Doolittle’s DH-4B-1-S at Kelly Field.

The Airco DH.4 was a very successful airplane of World War I, designed by Geoffrey de Havilland. It was built by several manufacturers in Europe and the United States. The DH-4B was a rebuilt DH.4 with fuel capacity increased to 110 gallons (420 liters). The DH-4B was 30 feet, 6 inches (9.296 meters) long with a wingspan of 43 feet, 6 inches (13.259 meters) and height of 10 feet, 4 inches (3.150 meters). Loaded weight of the standard DH-4B was 3,557 pounds (1,613.4 kilograms).

In place of the Rolls-Royce Eagle VII V-12 of the British-built version, Army Air Service DH-4s were powered by a water-cooled, normally-aspirated, 1,649.336-cubic-inch-displacement (27.028 liter) Liberty L-12 single overhead cam (SOHC) 45° V-12 engine with a compression ratio of 5.4:1. The Liberty produced 408 horsepower at 1,800 r.p.m. The L-12 as a right-hand tractor, direct-drive engine. It turned turned a two-bladed fixed-pitch wooden propeller. The Liberty 12 was 5 feet, 7.375 inches (1.711 meters) long, 2 feet, 3.0 inches (0.686 meters) wide, and 3 feet, 5.5 inches (1.054 meters) high. It weighed 844 pounds (383 kilograms).

The Liberty L12 aircraft engine was designed by Jesse G. Vincent of the Packard Motor Car Company and Elbert J. Hall of the Hall-Scott Motor Company. This engine was produced by Ford Motor Company, as well as the Buick and Cadillac Divisions of General Motors, The Lincoln Motor Company (which was formed by Henry Leland, the former manager of Cadillac, specifically to manufacture these aircraft engines), Marmon Motor Car Company and Packard. Hall-Scott was too small to produce engines in the numbers required.

This same airplane, DH.4B-1-S, A.S. No. 22-353, was flown from the Gulf of Mexico to the Canadian border by Lieutenant H.G. Crocker, 26 May 1923.

Lieutenant Doolittle's DH-4B-S-1 is serviced by maintenance technicians at Kelly Field, Texas.
Lieutenant Doolittle’s DH-4B-1-S is serviced by maintenance technicians at Kelly Field, Texas.
First Lieutenant James Harold Doolittle, Air Service, United States Army. “Jimmy Doolittle is wearing the Military Aviator badge and the World War I Victory Medal ribbon. (NASM/U.S. Air Force)

Jimmy Doolittle was one of America’s foremost pioneering aviators. He set many records, won air races, tested and developed new flying equipment and techniques. He was a highly-educated military officer, having earned his Bachelor of Arts from the University of California Berkeley School of Mines, and M.S and D.Sc. degrees in Aeronautical Engineering from the Massachusetts Institute of Technology.

During World War II Colonel Doolittle planned and led the famous Halsey-Doolittle Raid against Japan, 18 April 1942, for which he was awarded the Medal of Honor. As a brigadier general he commanded Twelfth Air Force in North Africa. Promoted to major general, he was given command of the Fifteenth Air Force in the Mediterranean Theater. From 1943 until 1945, Lieutenant General Doolittle commanded Eighth Air Force. He was preparing his command to move against Japan, equipped with Boeing B-29 Superfortress bombers when World War II came to an end.

Lieutenant General James H. Doolittle, commanding Eighth Air Force, in the cockpit of a Boeing B-29 Superfortess.

After the war, Lieutenant General Doolittle was placed on the inactive list. On 4 April 1985, by Act of Congress, James H. Doolittle was promoted to General.

General James Harold Doolittle is the only person to be awarded both the Medal of Honor and the Medal of Freedom. He died 27 September 1993 at the age of 96 years. He was buried at the Arlington National Cemetery, Arlington, Virginia.

Similar to the DH.4B-1-S flown by Lieutenant Jimmy Doolittle on his transcontinental flight, this is a reproduction DH.4B from the collection of the National Museum of the United States Air Force. (U.S. Air Force)

¹ Pablo Beach, Florida, was renamed Jacksonville Beach on 15 June 1925.

© 2018, Bryan R. Swopes

25 May 1927

1st Lieutenant James H. Doolittle, United States Army Air Corps, at the 1929 Cleveland National Air Races. Jimmy Doolittle is seen in this photograph sitting on the turtle deck of the Curtiss P-1C Hawk. (National Air and Space Museum)

25 May 1927: At Wright Field, now Wright-Patterson Air Force Base, Dayton, Ohio, First Lieutenant James H. “Jimmy” Doolittle, United States Army Air Corps, was the first pilot to successfully perform an outside loop.

Flying a Curtiss P-1B Hawk pursuit, he began the maneuver in level flight at 10,000 feet (3,048 meters), then pushed the nose down into a dive. When he reached 280 miles per hour (450 kilometers per hour), Doolittle continued to pitch the nose “down” and the airplane flew through a complete vertical circle, with the pilot’s head to the outside of the loop.

Lt. Jimmy Doolittle with a Curtiss P-1 Hawk, 4 February 1928. (NASM)
Lt. Jimmy Doolittle with a Curtiss P-1 Hawk, 4 February 1928. (National Museum of the United States Air Force)

Jimmy Doolittle attempted to repeat the outside loop at the 1929 Cleveland National Air Races, with a Curtiss P-1C Hawk, serial number 29-227. The airplane’s wings came off but Doolittle parachuted to safety. (The Curtiss P-1C used wing radiators instead of the large radiator under the nose of the P-1B. This substantially reduced the aerodynamic drag which allowed the airplane to accelerate to too high an airspeed during Doolittle’s maneuver.)

A crowd surrounds the wreckage of Jimmy Doolittle's Curtiss P-1C Hawk after it crashed during a demonstration at the 1929 Cleveland National Air Races. (Cleveland Press)
A crowd surrounds the wreckage of Jimmy Doolittle’s Curtiss P-1C Hawk after it crashed during an aerobatic demonstration at the 1929 Cleveland National Air Races. (Cleveland State University, Michael Schwartz Library, Special Collections, Cleveland Press Collection)

Jimmy Doolittle was one of America’s foremost pioneering aviators. He set many records, won air races, tested and developed new flying equipment and techniques. He was a highly-educated military officer, having earned his Bachelor of Arts from the University of California Berkeley School of Mines, and M.S and D.Sc. degrees in Aeronautical Engineering from the Massachusetts Institute of Technology. As a pioneer aviator, he won every international air race, and had been awarded every international aviation trophy. He was also the first pilot to fly completely by reference to instruments.

During the early days of America’s involvement in World War II, Lieutenant Colonel Doolittle planned and led the Halsey-Doolittle B-25 raid on Japan. He was awarded the Medal of Honor and promoted to brigadier general, and then placed in command of the Twelfth Air Force in North Africa. As a major general, he commanded the Fifteenth Air Force in the Mediterranean Theater of Operations. Lieutenant General Doolittle commanded the Eighth Air Force in England from January 1944 to September 1945. He supervised the transition of the 8th to the Boeing B-29 Superfortress and its eventual transfer to bases on Okinawa to continue the war against Japan. World War II came to an end before any of the 8th’s B-29s actually moved west.

Lieutenant General James H. Doolittle, U.S. Army Air Force (U.S. Army Photo C-2102)
Lieutenant General James H. Doolittle, U.S. Army Air Force (U.S. Army Photo C-2102)

After the war, Lieutenant General Doolittle was placed on the inactive list. On 4 April 1985, by Act of Congress, James H. Doolittle was promoted to General, United States Air Force, Retired.

General James Harold Doolittle is the only person to be awarded both the Medal of Honor and the Medal of Freedom. He died 27 September 1993 at the age of 96 years. He was buried at the Arlington National Cemetery, Arlington, Virginia.

Curtiss P-1B Hawk, A.C. 27-75. (U.S. Air Force)

The Curtiss P-1B Hawk was a single-engine, single-seat, single-bay biplane pursuit, an aircraft type now known as a fighter. The airplane and its D-12 Conqueror engine were both built by the Curtiss Aeroplane and Motor Co., Garden City, New York.

The P-1B was 22 feet, 10 inches (6.960 meters) long with an upper wingspan of 31 feet, 6 inches (9.601 meters). The lower wing had a span of 26 feet, 0 inches (7.925 meters), a narrower chord, and was staggered 3 feet, 2½ inches (0.978 meters) behind the upper. Both wings had significant taper with rounded tips. Their angle of incidence was 0°. The upper wing had no dihedral, while the inboard lower wing had 1°, and the outer, 5°. The total wing area was 252 square feet (23.4 square meters). The horizontal stabilizer span was 10 feet, 6.0 inches (3.200 meters) and its incidence could be adjusted from +3° to -1.5°. The vertical fin was offset 2° left of the airplane’s centerline. The overall height of the airplane was 8 feet, 10 inches (2.712 meters).

The P-1B had an empty weight of 2,105 pounds (955 kilograms), gross weight of 2,932 pounds (1,330 kilograms), and maximum weight of 3,562 pounds ( kilograms).

The P-1B was powered by a liquid-cooled, normally-aspirated, 1,145.1-cubic-inch-displacement (18.8 liter) Curtiss D-12D (V-1150-3) dual overhead cam (DOHC) 4-valve 60° V-12 engine with a compression ratio of 5.7:1. It was a direct-drive engine, rated at 415 horsepower at 2,000 r.p.m. at Sea Level, and 460 horsepower at 2,300 r.p.m. The D-12 was 58¾ inches (1.492 meters) long, 34¾ inches (0.883 meters) high and 28¼ inches (0.718 meters) wide. It weighed 680 pounds (308 kilograms). The P-1B was equipped with an aluminum Curtiss-Reed propeller with a diameter of 8 feet, 9 inches (2.667 meters).

The pursuit had a cruise speed of 127 miles per hour (204 kilometers per hour). Its maximum speed was 159.6 miles per hour (256.9 kilometers per hour) at Sea Level, and 157 miles per hour (253 kilometers per hour) at 5,000 feet (1,524 meters). It had a service ceiling of 21,400 feet (6,523 meters) and absolute ceiling of 22,900 feet (6,980 meters). Its range was 342 miles (550 kilometers).

The P-1B was armed with two fixed air-cooled Browning machine guns, one .50-caliber and one .30-caliber.

The Air Corps ordered 93 Curtiss P-1 Hawks between 1925 and 1929.

Doolittle flew a Curtiss Curtiss P-1A Hawk, 25-410, similar to the P-1B that Doolittle flew into an outside loop. (U.S. Air Force)
Curtiss P-1A Hawk, 25-410, similar in appearance to the P-1B that Doolittle flew into an outside loop. (U.S. Air Force)

© 2018, Bryan R. Swopes