Boeing B-29-40-BW Superfortress 42-24612. (U.S. Air Force)
4 November 1954: The Strategic Air Command retired its last B-29 Superfortress four-engine heavy bomber to the aircraft storage facility at Davis-Monthan Air Force Base, Tucson, Arizona.
The B-29 Superfortress was the most technologically advanced—and complex—aircraft of World War II. It required the manufacturing capabilities of the entire nation to produce. Over 1,400,000 engineering man-hours had been required to design the prototypes.
The Superfortress was manufactured by Boeing at Seattle and Renton, Washington, and Wichita, Kansas; by the Glenn L. Martin Company at Omaha, Nebraska; and by Bell Aircraft Corporation, Marietta, Georgia.
There were three XB-29 prototypes, 14 YB-29 pre-production test aircraft, 2,513 B-29 Superfortresses, 1,119 B-29A, and 311 B-29B aircraft. The bomber served during World War II and the Korean War and continued in active U.S. service until 1960. In addition to its primary mission as a long range heavy bomber, the Superfortress also served as a photographic reconnaissance airplane, designated F-13, a weather recon airplane (WB-29), and a tanker (KB-29).
The B-29 was operated by a crew of 11 to 13 men. It was 99 feet, 0 inches (30.175 meters) long with a wingspan of 141 feet, 3 inches (43.068 meters). The vertical fin was 27 feet, 9 inches (8.305 meters) high. Empty weight was 74,500 pounds (33,793 kilograms) with a maximum takeoff weight of 133,500 pounds (60,555 kilograms).
The B-29 was powered by four air-cooled, supercharged, 3,347.66-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division Cyclone 18 (also known as the Duplex-Cyclone) 670C18BA4 (R-3350-23A) two-row 18-cylinder radial engines, which had a Normal Power rating of 2,000 horsepower at 2,400 r.p.m., and 2,200 horsepower at 2,800 r.p.m. for takeoff. They drove 16 foot, 7 inch (5.055 meter) diameter, four-bladed, Hamilton Standard constant-speed propellers through a 0.35:1 gear reduction. The R-3350-23A was 6 feet, 4.26 inches (1.937 meters) long, 4 feet, 7.78 inches (1.417 meters) in diameter and weighed 2,646 pounds (1,200 kilograms).
The maximum speed of the B-29 was 357 miles per hour (575 kilometers per hour) at 30,000 feet (9,144 meters), though its normal cruising speed was 220 miles per hour (354 kilometers per hour) at 25,000 feet (7,620 meters). The bomber’s service ceiling was 33,600 feet (10,241 meters) and the combat range was 3,250 miles (5,230 kilometers).
The Superfortress could carry a maximum of 20,000 pounds (9,072 kilograms) of bombs in two bomb bays. For defense it had 12 Browning M2 .50-caliber machine guns in four remote-controlled turrets and a manned tail position.
A number of B-29 Superfortresses are on display at locations around the world, but only two, the Commemorative Air Force’s B-29A-60-BN 44-62070, Fifi, and B-29-70-BW 44-69972, Doc, are airworthy. (After a lengthy restoration, Doc received its Federal Aviation Administration Special Airworthiness Certificate, 19 May 2016.)
The Superfortress could carry a maximum of 20,000 pounds (9,072 kilograms) of bombs in two bomb bays. For defense it had 12 Browning M2 .50-caliber machine guns in four remote-controlled turrets and a manned tail position.
B-29 Superfortresses in storage at Davis-Monthan Air Force Base. (LIFE Magazine)
Boeing 314, California Clipper, NC18602, over Oakland, California, 1937. Photographed for Pan Am by Clyde Herwood Sunderland, Jr. (1900–1989).(Clyde Sunderland Photograph Collection, Library, University of California Berkeley)
3–4 November 1945: On the evening of Saturday, 3 November 1945, the Boeing 314 Honolulu Clipper, NC18601, departed Honolulu, Oahu, Territory of Hawaii, enroute to San Francisco, California. The flying boat was under the command of Captain Sanis E. (“Robby”) Robbins, Pan American Airways, with First Officer Wally Reed, Second Officer Dunbar Carpenter, Radio Officer Jack B. Crawford, First Engineer Dan W. Broadwater, Second Engineer Robert J. Dernberger. There were 13 passengers and 10 crew members on board. The flight to San Francisco was expected to take 11 hours.
Approximately 5 hours into the flight, the number 3 engine (starboard wing, inboard) began to backfire. It was shut down and the propeller feathered. Captain Robbins decided to return to Hawaii. A short while later, the number 4 engine (starboard wing, outboard) also started to malfunction. It continued to run but eventually it was also shut down.
With two engines inoperative, the airplane was unable to maintain altitude. At 11:07 p.m. local, Captain Robbins, in total darkness, brought the flying boat to a “masterful” landing on the relatively calm surface of the Pacific Ocean. There were no injuries. The airplane suffered minor damage to the port sea wing, and started taking on water.
California Clipper, NC18602, another Boeing 314, also enroute to San Francisco, orbited Honolulu Clipper‘s position to guide rescue ships to scene. The following message was broadcast from Pearl Harbor:
PAN AMERICAN CLIPPER DOWN AT SEA AT 040935Z POSITION 2749N 14802W. PLANE IN GOOD CONDITION. IS ABLE TO COMMUNICATE ON [frequency deleted] KCS VOICECALL C18601 ON [frequency deleted] KCS. INVESTIGATE SIGHTINGS REPORT PERTINENT INFO TO ORIGINATOR.
The United States Army transport ship, U.S.A.T. John Henry Payne sighted flares fired from the flying boat and quickly arrived on scene. The ship took all of the passengers on board. Ten crew stayed aboard flying boat.
USS Manila Bay (CVE 61), a Casablanca-class escort aircraft carrier under the command of Captain Leon Johnson, was approximately 60 miles (97 kilometers) away, and had been ordered to take charge of efforts to salvage the airplane.
On arrival, a whale boat was sent to remove the remaining crew members from the flying boat. Wind and waves had increased and it was feared that the boat might damage the hull of the flying boat, so a rubber life raft was used to transfer the Clipper‘s crew to the whale boat. Aircraft mechanics were sent from Manila Bay to attempt to repair the airplane, but were not successful.
A whale boat from USS Manila Bay approaches Honolulu Clipper, 4 November 1945. (U.S. Navy)
Plans were made to rig the airplane for towing. 200 fathoms (1,200 feet/366 meters) of 6-inch (15.2 centimeter) diameter hawser was rigged from the aircraft carrier to the nose of the flying boat. Stabilizing lines were tied to the propeller hubs of the outboard engines. Manila Bay began towing the Honolulu Clipper and was gradually able to increase speed to 6 knots (7 miles per hour/11 kilometers per hour). About an hour after sunset, at about 7:30 p.m., the tow line parted.
Darkness and rising seas made it impossible to rig a new tow. Manila Bay stood by awaiting arrival of USS San Pablo (AVP-30) (Commander Charles Robert Eisenbach), a Barnegat-class seaplane tender, on Tuesday, 6 January, then departed for Pearl Harbor.
Seaplane tender USS San Pablo (AVP-30) standing by Honolulu Clipper. (U.S. Navy)USS San Pablo approaches the undamaged Honolulu Clipper. (U.S. Navy)
During the several days that Honolulu Clipper was afloat in the open ocean, weather increased to the point that it was considered too hazardous to approach it in a small boat, so the aviation tender closed on the airplane directly to try to take it on tow. Unfortunately, San Pablo hit the clipper and caused significant damage.
Hawaii Clipper from the bridge of USS San Pablo. The starboard wing is damaged and the Number 4 engine is missing. (U.S. Navy)
With salvage impossible, the derelict Honolulu Clipper was now considered a hazard to navigation. It was sunk by 20 mm gun fire from San Pablo.
Honolulu Clipper was the prototype for the Boeing Model 314 series flying boat. It had been designed to carry a maximum of 76 passengers and a crew of 10 a distance of 5,200 miles at 184 miles per hour. The design used the wings and engine nacelles of Boeing’s experimental Model 294 (XB-15) very long-range heavy bomber.
The Boeing Model 314 was a large four-engine, high-wing monoplane flying boat designed and built by the Boeing Airplane Company to take off and land on water. It was 106 feet (32.309 meters) long with a wingspan of 152 feet (46.330 meters). It had a maximum take off weight of 82,500 pounds (37,421 kilograms).
Boeing 314 prototype NX18601 in original configuration. (Boeing Airplane Company)
The airplane was built at Boeing’s Plant 1, then transported by barge to Elliot Bay. It carried experimental registration NX18601. Test pilot Edmund Turney (“Eddie”) Allen made the first flight of the prototype on 7 June 1938. He reported that the flying boat had insufficient rudder control and that he had to vary engine power to turn it. The prototype was modified to a twin-tail configuration.
Boeing Model 314 NX18601 flying over Elliot Bay. Note the twin-tail configuration. (Boeing Airplane Company)
With two vertical fins and rudders, control was improved, but was still insufficient. A third, center, fin was added and this became the production configuration.
Prototype Boeing 314 NX18601 in triple-tail configuration, 24 November 1938. (U.S. Air Force/San Diego Air and Space Museum)
The Boeing 314 was powered by four air-cooled, supercharged, 2,603.737-cubic-inch-displacement (42.668 liter) Wright Aeronautical Division Cyclone 14 GR2600A2, two-row, 14-cylinder radial engines with a compression ratio of 7.1:1. They were rated at 1,200 horsepower at 2,100 r.p.m., and 1,550 horsepower at 2,400 r.p.m. for takeoff, burning 91/96 octane gasoline. These engines (also commonly called “Twin Cyclone”) drove three-bladed Hamilton Standard Hydromatic full-feathering constant-speed propellers with a diameter of 14 feet (4.267 meters) through a 16:9 gear reduction. The GR2600A2 was 5 feet, 2.06 inches (1.576 meters) long and 4 feet, 7 inches (1.387 meters) in diameter. It weighed 1,935 pounds (878 kilograms). The engines could be serviced in flight, with access through the wings.
The Boeing 314 had a maximum speed of 199 miles per hour (320 kilometers per hour), with a range of 3,685 miles (5,930 kilometers) at its normal cruising speed of 183 miles per hour (295 kilometers per hour). Its service ceiling was 13,400 feet (4,084 meters). The fuel capacity was 4,246 gallons (16,073 liters).
Boeing built six Model 314 and another six 314A flying boats for Pan American Airways and British Overseas Airways Corporation. Pan Am paid $549,846.55 for each 314, about $9,545,726.07 in 2017 dollars, and Boeing lost money on every one sold.
Honolulu Clipper was leased to the United States Navy by Pan American Airways, 17 December 1942, and assigned Bureau of Aeronautics serial number (“Bu. No.”) 48227. The airplane continued to be operated by Pan Am crews.
A Pan American Airways Boeing 314 at Hawaii. (San Diego Air and Space Museum)
Sanis E. (“Robby”) Robbins was born at Matthews, Indiana, 17 September 1898. He was the sixth of seven children of William S. Robbins, a real estate agent, and Sarah Ellen Brokaw Robbins.
Robbins enlisted as a Private, United States Army, at Camp Dodge, Iowa, 26 June 1916. He was promoted to Private First Class on 1 August 1916, and to Corporal, 18 December 1916. Corporal Robbins was hospitalized at Brownsville, Texas, 4–23 January 1917. He was released from military service at Fort Des Moines, Iowa, 20 February 1917, shortly before the United States entered World War I. A 1920 Air Service Information Circular listed Second Lieutenant Sanis E. Robbins as a pursuit pilot, residing at Cassia, Florida.
Robby Robbins married Miss Virginia J. Bing. They would have three children.
Robbins was commissioned as a Lieutenant Commander, United States Naval Reserve, 15 September 1940. He held this rank until at least 1955.
Captain Sanis E. Robbins died at Palo Alto, California, 8 August 1961, at the age of 62 years. He was buried at the Golden Gate National Cemetery, San Bruno, California.
Pan American Airways Boeing 314 NC18604, Atlantic Clipper, taking off. (NASM)
Lockheed YP-38 Lightning 39-689, manufacturer’s serial number 122-2202. (Lockheed Martin)Ralph Burwell. Virden (Los Angeles Times)
4 November 1941: Lockheed test pilot Ralph Burwell Virden was conducting high speed dive tests in the first Lockheed YP-38 Lightning, Air Corps serial number 39-689 (Lockheed’s serial number 122-2202).
As the airplane’s speed increased, it approached what is now known as its Critical Mach Number. Air flowing across the wings accelerated to transonic speeds and began to form shock waves. This interrupted lift and caused a portion of the wing to stall. Air no longer flowed smoothly along the airplane and the tail surfaces became ineffective. The YP-38 pitched down into a steeper dive and its speed increased even more.
Designed by famed aeronautical engineer Clarence L. “Kelly” Johnson, the YP-38 had servo tabs on the elevator that were intended to help the pilot maintain or regain control under these conditions. But they increased the elevator’s effectiveness too well.
The Los Angeles Times described the accident:
Witnesses said the twin-engined, double-fuselaged ship was booming westward at near maximum speed (unofficially reported to be between 400 and 500 miles an hour) when the duralumin tail assembly “simply floated away.”
A moment afterward the seven-ton craft seemed to put on a burst of speed, the the high whine of its engines rising.
It then went into a downward glide to about 1500 feet, then into a flat spin, flipped over on its back and shot earthward.
Several persons said that they thought they had heard an explosion during the dive, but qualified observers doubted it. . .
. . . Fellow pilots at Lockheed said, “Ralph was the best we had, especially in power dives.”
Robert E. Gross, president of Lockheed, said, “Ralph Virden was a great pilot but an even greater man. If anyone ever had national defense at heart it was he, who every day was carrying the science of aviation into new and higher fields.”
Various witnesses said the ill-fated ship’s tail assembly could be followed easily as its bright surfaces glinted in the sun during its drop to earth. It landed several blocks from the scene of the crash.
Mrs. Jack Davenport of 1334 Elm Ave., left her ironing board when she heard the unfamiliar roar of the plunging plane’s engines.
“I ran out and saw it passing over us, very low. It disappeared among the trees and then zoomed back into sight just before crashing in the next block,” she said. “It looked just like a toy airplane. I knew the pilot didn’t have a chance, as the ship was too low and going too fast.”
—Los Angeles Times, Vol. LX, Wednesday, 5 November 1941, Page 1, Column 6, and Page 2, Column 5.
The YP-38 crashed into the kitchen of Jack Jensen’s home at 1147 Elm Street, Glendale, California. Fire erupted. Ralph Virden was killed. The airplane’s tail section was located several blocks away.
Another photograph of Lockheed YP-38 Lightning 39-689. The factory serial number, “2202,” is stenciled on the nose. (Lockheed Martin)
39-689 was the first of thirteen YP-38 service test aircraft that had been ordered by the U.S. Army Air Corps shortly after the XP-38 prototype, 37-457, had crashed on a transcontinental speed record attempt, 11 February 1939. 39-689 made its first flight 16 September 1940 with test pilot Marshall Headle at the controls. With hundreds of production P-38s being built, Lockheed continued to use the YP-38 for testing.
Newspaper photograph of the wreckage of Lockheed YP-38 Lightning 39-689 at 1147 Elm Street, Glendale, California. (Los Angeles Times)
The YP-38s were service test prototypes of a single-place, twin engine long range fighter with a unique configuration. There was not a fuselage in the normal sense. The cockpit, nose landing gear, and armament were contained in a central nacelle mounted to the wing. Two engines and their turbochargers, cooling systems and main landing gear were in two parallel booms. The booms end with vertical fins and rudders, with the horizontal stabilizer and elevator between them. The P-38 was 37 feet, 9–15/16 inches (11.530 meters) long, with a wingspan of 52 feet, 0 inches (15.850 meters) and height of 12 feet, 10 inches (3.952 meters).
The P-38’s wings had a total area of 327.50 square feet (30.43 square meters). Their angle of incidence was 2° and there was 5° 40′ dihedral. The leading edges were swept aft 5° 10′.
The YP-38 had an empty weight 11,171 pounds (5,067 kilograms). The gross weight was 13,500 pounds (6,123 kilograms) and the maximum takeoff weight 14,348 pounds (6,508 kilograms).
The YP-38 was powered by two counter-rotating, liquid-cooled, turbosupercharged 1,710.597-cubic-inch displacement (28.032 liter) Allison V-1710-27 right-hand tractor and V-1710-29 left-hand tractor, single overhead cam (SOHC) 60° V-12 engines (Allison Engineering Co. Models F2R and F2L) with a Normal Power rating of 1,000 horsepower at 2,600 r.p.m., and 1,150 horsepower at 3,000 r.p.m. for takeoff. They drove three-bladed Curtiss Electric constant-speed propellers with a diameter of 11 feet, 6 inches (3.505 meters) through a 2.00:1 gear reduction. In a change from the XP-38, the propellers rotated outboard at the top of their arc. The V-1710-27/-29 engines were 7 feet, 1-5/8 inches (2.175 meters) long, 2 feet, 5-9/32 inches (0.744 meters) wide and 3 feet, 0-17/32 inches (0.928 meters) high. The V-1710-27/-29 weighed 1,305 pounds (592 kilograms)
The YP-38 had a maximum speed of 405 miles per hour (651.8 kilometers per hour) at 10,000 feet (3,048 meters) and it could climb from the surface to 20,000 feet (6,096 meters) in six minutes. Normal range 650 miles (1,046 kilometers).
Lockheed built one XP-38, thirteen YP-38s, and more than 10,000 production fighter and reconnaissance airplanes. At the end of World War II, orders for nearly 2,000 more P-38 Lightnings were cancelled.
Lockheed YP-38 39-692 in flight.(Hans Groenhoff Photographic Collection, Smithsonian Institution National Air and Space Museum NASM-HGC-967)
Ralph Burwell Virden was born 11 June 1898, at Audobon Township, Illinois. He was the second child of Hiram R. Virden, a farmer, and Nancy Carrie Ivy Virden.
Virden attended Bradley Polytechnic Institute at Peoria, Illinois. At the age of 17, 15 October 1918, Ralph Virden enlisted in the U.S. Army. With the end of World War I less than one month later, he was quickly discharged, 7 December 1918.
In 1919, Ralph Virden married Miss Florence I. McCullers. They would have two children, Kathryn and Ralph, Jr. Kathryn died in 1930 at the age of ten years.
Ralph Burwell Virden with a Boeing Model 40 mail plane, circa late 1920s. As a U.S. Air Mail pilot, Virden is armed with a .45-caliber Colt M1911 semi-automatic pistol. (San Diego Air and Space Museum Archives)Boeing Airplane Company President Clairmont L. Egvtedt and United Air Lines Captain Ralph B. Virden examine a scale model of the Boeing 247D airliner. (Boeing)
During the mid-1920s, Virden flew as a contract mail pilot. He held Airline Transport Pilot Certificate No. 628, and was employed by Gilmore Aviation and Pacific Air Transport. For thirteen years, Virden was a pilot for United Air Lines. He joined Lockheed Aircraft Company as a test pilot in 1939. He had flown more than 15,000 hours.
Virden lived at 4511 Ben Ave., North Hollywood, California, with his family. Ralph, Jr., now 19 years of age, was also employed at Lockheed. (Following his father’s death, the younger Virden enlisted in the United States Navy.)
After the accident, Lockheed, the Air Corps and the National Advisory Committee on Aeronautics (NACA) undertook an extensive test program of the P-38.
The second Lockheed YP-38 Lightning, 39-690, was sent to the NACA Langley Research Center at Langley Field, Virginia. This photograph is dated 4 February 1942. (NASA)Lockheed YP-38 39-690 in the NACA Full Scale Tunnel, December 1944. (NASA)Lockheed YP-38 Lightning 39-690, serial number 122-2203. (NASA)Lockheed YP-38 Lightning, 39-690 (122-2203), in the NACA Langley Research Center’s full-scale wind tunnel at Langley Field, Virginia, December 1944. (NASA)Lockheed YP-38 Lightning 39-690. (NASA)Lockheed YP-38 Lightning 39-690. (NASA)Lockheed YP-38 Lightning 39-690. (NASA)Lockheed YP-38 Lightning 39-690, 122-2203. (NASA)
4 November 1927: At Venezia, Mario de Bernardi flew a Macchi M.52 seaplane to a new Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course of 479.29 kilometers per hour (297.82 miles per hour).¹
Macchi M.52 number 7. (San Diego Air and Space Museum Archive)
Aeronautica Macchi built three M.52 seaplanes for the Regia Aeronautica (the Italian Air Force) for use in the 1927 Schneider Trophy Races. The M.52 was designed by Mario Castoldi. Like the earlier M.39, it was a single-place, single-engine, low-wing monoplane float plane constructed of wood and metal.
The three racers were each powered by a 2,116.14-cubic-inch-displacement (34.677 liter) liquid-cooled Fiat Aviazone AS.3 dual overhead camshaft, four-valve 60° V-12 engine which produced 1,000 horsepower at 2,400 r.p.m. The design of the AS.3 was based on the Curtiss D-12, although it used individual cylinders and water jackets instead of the American engine’s monoblock castings.
With its cowlings removed, the 1,000 horsepower Fiat AS.3 DOHC V-12 engine of the Macchi M-52 is visible. (San Diego Air and Space Museum Archive)
Hawthorne C. Gray, U.S. Army Air Corps, preparing for his balloon ascent at Scott Field, Illinois, 4 November 1927. (U.S. Air Force)
4 November 1927: Captain Hawthorne C. Gray, United States Army Air Corps, a balloon pilot since 1921, has carried out a series of ascents to study the effects of very high altitude on air crews.
Gray lifted off from Scott Field, Belleville, Illinois, at 2:13 p.m., in a helium-filled balloon with an open wicker gondola suspended below. The balloon, Air Corps serial number S 30-241, was constructed of rubberized silk and coated with aluminum paint. It had a volume of 70,000 cubic feet (1,982.2 cubic meters). In the gondola were instruments for measuring altitude and temperature, as well as two sealed recording barographs provided by the National Aeronautic Association (NAA). Captain Gray was dressed in heavy leather clothing for protection against the cold. Three gas cylinders of oxygen were provided for breathing at altitude.
This photograph of the equipment carried in Hawthorne’s gondola on 4 November 1927 shows the three oxygen cylinders and breathing mask. (U.S. Air Force)
Early in the ascent, high winds carried him to the south, and though he was accompanied by four airplanes, their pilots quickly lost sight of Gray’s balloon. It disappeared into a heavy overcast 20 minutes after takeoff and rose to a peak altitude of 42,470 feet (12,944.9 meters) at 4:05 p.m.
Based on Captain Gray’s notes and data from the barographs, it was concluded that his ascent was at a much slower rate than his previous altitude flights. At 3:17 p.m., he wrote “Clock frozen.” Without the clock, Gray was unable to calculate his time aloft and the amount of breathing oxygen remaining. Estimates prior to lift off were that the supply would run out at 4:38 p.m. The balloon had only descended to 39,000 feet (11,887 meters) by 4:28 p.m. The barographs showed an increase in rate of descent at this time, indicating that Captain Gray was venting helium from the balloon to try to descend faster. The descent slowed, however, suggesting that Gray had lost consciousness.
Captain Hawthorne C. Gray, USAAC, right, wearing flight suit, with Lieutenant Colonel John Albert Paegelow. (San Diego Air and Space Museum Archives)
The balloon and gondola were found near Sparta, Tennessee at 5:20 p.m., with Hawthorne Gray’s body curled in the bottom of the gondola. Captain Gray suffered a loss of oxygen which resulted in his death.
Captain Gray was awarded the Distinguished Flying Cross, posthumously, and is buried at the Arlington National Cemetery.
His citation reads:
The President of the United States of America, authorized by Act of Congress, July 2, 1926, takes pride in presenting the Distinguished Flying Cross (Posthumously) to Captain (Air Corps) Hawthorne C. Gray, U.S. Army Air Corps, for heroism while participating in an aerial flight. On 9 March 1927, Capitan Gray attempted to establish the World’s altitude record for aircraft, but due to the faulty oxygen apparatus he fainted at an altitude of 27,000 feet recovering consciousness after 52 minute, when his balloon, having over shot its equilibrium point, descended to an atmosphere low enough to sustain life. Undaunted by this experience, Captain Gray on 4 May 1927, made a record attempt when he attained an altitude of 42,470 feet, higher than any other Earth creature has ever gone. On his descent, however, his balloon failed to parachute, and it was necessary for him to descend from 8,000 feet in a parachute. With faith unshaken, and still displaying great courage and self reliance, Capitan Gray, on 4 November 1927, made the third attempt, which resulted in his making the supreme sacrifice. Having attained an altitude of 42,000 feet he waited for ten minutes, testing his reactions, before making a last rapid climb to his ceiling and a more rapid descent to safe atmosphere. Undoubtedly his courage was greater than his supply of oxygen, which gave out at about 37,000 feet.
War Department, General Orders No. 5 (1928)
The wicker balloon gondola used by Captain Hawthorne C. Gray on 4 November 1927, on display at the Smithsonian Institution National Air and Space Museum. (NASM)
Hawthorne Charles Gray was born at Pasco, Washington, 16 February 1889. He was the fourth of six children of William Polk Gray, a river steamboat pilot, and Oceanna (“Ocia”) Falkland Gray.
In 1913, Gray was employed as a baggageman for the Northern Pacific Railway at the Pasco Station. Gray attended University of Idaho at Moscow, Idaho, as a member of the Class of 1913. He graduated with a Bachelor of Science degree in Electrical Engineering, B.S.(E.E.)
Hawthorne C. Gray served as an enlisted soldier with the 1st Battalion, 2nd Infantry, Idaho National Guard, 1911–1912, a second lieutenant, 25th Infantry, Idaho National Guard, from 7 March 1912 to 23 April 1913. He was qualified as an Expert Rifleman. Gray enlisted in the United States Army, serving in the Hospital Corps and Quartermaster Corps from 19 January 1915 to 25 June 1917. He participated in the Mexican Expedition, under General John J. Pershing.
Sergeant Senior Grade Gray was commissioned as a second lieutenant, 32nd Infantry, 3 June 1917, and promoted to 1st lieutenant on the same day. Lieutenant Gray was promoted to captain (temporary), 34th Infantry, on 5 August. The rank of captain became permanent on 24 February 1920.
Captain Hawthorne Charles Gray, Air Service, United States Army, circa 1923.
Captain Gray was assigned to duty with the Air Service from 9 August 1920, and was transferred to that branch was transferred on 29 August 1921. His date of rank was retroactive to 21 February 1920. Gray graduated from the Army’s Balloon School, Ross Field, in 1921. In 1923 graduated from the Air Service Primary Flying School at Brooks Field, Texas, in 1923, and from the Balloon and Airship School at Scott Field in 1924.
Captain Gray and Mrs. Gray traveled to Europe to participate in the 15th Coupe Aéronautique Gordon Bennett (the Gordon Bennett Cup balloon race), held 30 May 1926 at Wilrijck, a small city near Antwerp, Belgium. Gray and his team mate, Lieutenant Douglas Johnson, placed second out of eighteen competitors, and behind another American team. Gray and Johnson traveled 599 kilometers (964 statute miles) in 12:00 hours, landing in the Duchy of Meklenburgia, a free state of the Weimar Republic (northern Germany), at about 4:00 a.m., 31 May. The Grays returned to the United States, arriving aboard S.S. President Harding at New York City after an eight-day voyage from Cherbourg, on 23 July 1926.
Captain Gray reached an altitude of 8,690 meters (28,510.5 feet) over Scott Field on 9 March 1927. This ascent set three Fédération Aéronautique Internationale (FAI) World Records for Altitude. ¹ On 4 May 1927, Captain Gray reached approximately 42,240 feet (12,875 meters). Because of a high rate of descent, he parachuted from the gondola at about 8,000 feet (2,438 meters). Because he was not on board at the landing, the Fédération Aéronautique Internationale (FAI) did not recognize the flight as an official altitude record.
Captain Gray was married to the former Miss Miriam Lorette Maddux of Santa Rosa, California. They would have four children. Their first died at the age of 1 year, 3 months.
¹ FAI Record File Numbers: 10614, Ballooning, Subclass A-6th; 10615, Ballooning, Subclass A-7th; Ballooning, Subclass A-8th.
