Bryan Allen flies Gossamer Albatross across the English Channel. (Don Monroe via Bryan Allen)
12 June 1979: The human-powered airplane, Gossamer Albatross, built by AeroVironment, Inc., of Simi Valley, California, flew across the English Channel from The Warrens, near Folkstone, Kent, England, to Cap Griz-Nez, France, 22.26 miles (35.82 kilometers) in 2 hours, 49 minutes.
The pilot/powerplant of Gossamer Albatross was long-distance bicyclist Bryan Lewis Allen. Allen pedaled at a constant 75 r.p.m. He established two Fédération Aéronautique Internationale (FAI) World Record: Straight Distance, 35.82 kilometers (22.26 miles)¹ ; Duration, 2 hours, 49 minutes.²
Bryan Lewis and Paul MacCready, London, 16 May 1979. (Getty Images/United News/Popperfoto)Gossamer Albatross arrives at France, 12 June 1978. (AeroEnvironment, Inc.
The aircraft was designed by Paul Beattie MacCready, Jr., Ph.D., and weighed just 70 pounds (31.8 kilograms), empty.
The two-way radio link failed right after takeoff. Unexpected winds made the flight an hour longer than planned and Allen used all of his water. Batteries powering the instruments ran down. A chase boat was prepared for Allen to abort the flight, but he continued to France.
Bryan Lewis Allen was born 13 October 1952 at Tulare, California. He attended Tulare Union High School and then College of the Sequoias and California State University, Bakersfield, earning a bachelor of science degree. Allen is employed as a software engineer for the Mars Reconnaissance Orbiter at the NASA Jet Propulsion Laboratory, Pasadena, California.
Paul Beattie MacCready, Jr., was born 29 September 1925. He graduated from Yale University with a bachelor’s degree in physics, and then earned a master’s in physics from the California Institute of Technology, Pasadena, California. In 1952, Caltech awarded MacReady a doctorate in aeronautics.
The Robert J. Collier Trophy. (Smithsonian Institution, National Air and Space Museum)
Dr. MacReady received the Collier Trophy for 1979 from the National Aeronautic Association, “For the concept, design and construction of the Gossamer Albatross, which made the first man-powered flight across the English Channel—with special recognition to Bryan Allen, the pilot.”
Dr. Paul B. MacReady died 25 August 2007 at Pasadena, California.
The Gossamer Albatross is a human-powered high-wing canard monoplane constructed primarily of carbon fiber tubing, expanded polystyrene foam, Mylar® and Kevlar®, with wire bracing. A single pilot in a gondola provides power to a two-bladed fixed-pitch propeller, pedaling at 75 r.p.m., through a bicycle-type gear-reduction drive mechanism.
The airplane is 50 feet, 6 inches (15.392 meters) long, with a wingspan of 93 feet, 10 inches (28.600 meters) and overall height of 16 feet, 4 inches (4.978 meters). It has an empty weight of 70 pounds (31.8 kilograms), and a gross weight at takeoff of 215 pounds (97.5 kilograms). Its maximum speed is 15 miles per hour (24 kilometers per hour).
Three-view drawing of Gossamer Albatross. (Natural Flight Foundation)
Gossamer Albatross is in the collection of the Stephen F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum.
Gossamer Albatross at the National Air and Space Museum. (NASM)
CAPT Walter W. Irwin lands at Edwards Air Force Base, California, 16 May 1958. The airplane is Lockheed F-104A-1-LO 55-2969. (U.S. Air Force)
16 May 1958: At Edwards Air Force Base, in the high desert of southern California, Captain Walter Wayne Irwin, United States Air Force, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15-to-25 Kilometer Straight Course when he flew a Lockheed F-104A Starfighter, serial number 55-2969, to 2,259.538 kilometers per hour (1,404.012 miles per hour). ¹ He made two runs over the course at an altitude of 40,000 feet (12,192 meters). ²
On the same day, Captain Irwin set two U.S. National Aeronautic Association time-to-altitude records by flying -969 to 3,000 meters in 41.8 seconds, and to 25,000 meters in 4 minutes, 26.03 seconds. It reached a peak altitude of 27,813 meters (91,246 feet).
Captain Walter W. Irwin, United States Air Force, stands next to a Lockheed F-104. (U.S. Air Force)
Captain Irwin was part of a group of engineers and pilots awarded the Robert J. Collier Trophy by the National Aeronautic Association in 1958 for “the greatest achievement in aeronautics” because of their involvement in the Lockheed F-104 program. In a ceremony held 16 December 1958, General Benjamin Wilkey Chidlaw, former commanding general, Air Defense Command, presented the Thompson Trophy to Captain Irwin.
Vice President Richard M. Nixon presents the Collier Trophy. Left to right, Major Walter W. Irwin and Lieutenant Colonel Howard C. Johnson; Nixon; Neil Burgess and Gerhard Neumann, designers of the General Electric J79 engine; and Clarence Leonard (“Kelly”) Johnson, Lockheed Aircraft Corporation. 15 December 1959. (NASM-00142388)Captain Walter W. Irwin, U.S. Air Force, at Edwards AFB, 16 May 1958. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
Walter Wayne Irwin was born 21 August 1924 at Everett, Washington. He was the son of John Harve Irwin, a shoe store clerk, and Stella Mildred Faulstich. He attended Wenatchee High School in Wanatchee, Washington, graduating in 1941.
Irwin enlisted as a private in the Air Corps, United States Army, at Seattle, Washington, 6 January 1942. Trained as a fighter pilot, he was commissioned as a second lieutenant 3 November 1942.
Lieutenant Irwin flew 88 combat missions in the Republic P-47 Thunderbolt with the Ninth Air Force in Europe during World War II. He was shot down, captured and held as a prisoner of war for a week before he escaped and made his way to friendly forces.
Captain Irwin married Lieutenant Christine Ann Stevens, Nurse Corps, United States Air Force, in a Catholic ceremony at Arlington, Virginia, 4 December 1954. Lieutenant Stevens was assigned to the base hospital at Travis Air Force Base in California. They would have four children.
At the time he set the record, Captain Irwin had just returned from an overseas assignment in Taiwan. He was a flight commander with the 83rd Fighter Interceptor Squadron, based at Hamilton Air Force Base, Novato, California.
In addition to the Collier Trophy, Major Irwin won the Thompson Trophy for his F-104 speed record.
Lockheed F-104A Starfighter 55-2969. The prototype Lockheed Model 188 Electra is in the photograph behind the interceptor.
Walter Irwin retired from the Air Force with the rank of colonel following thirty years of service. In retirement, he was owner of a realty company in Sebastopol, California.
On 17 April 1978, Colonel Irwin was flying a rented Piper PA-28-161 Cherokee Warrior near Occidental, California. Witnesses saw the airplane maneuvering at low altitude. A wing clipped an oak tree. The airplane crashed and caught fire. Walter Wayne Irwin was killed. His ashes were spread at sea.
Formation of two Lockheed F-104A-15-LO (S/N 56-0769 and 56-0781). (U.S. Air Force photo)
The Lockheed F-104A Starfighter was a single-place, single engine supersonic interceptor. It was designed by a team lead by the legendary Clarence L. “Kelly” Johnson.
The F-104A is 54.77 feet (16.694 meters) long with a wingspan of 21.94 feet (6.687 meters) and overall height of 13.49 feet (4.112 meters). The total wing area is just 196.1 square feet (18.2 square meters). At 25% chord, the wings are swept aft 18° 6′. They have 0° angle of incidence and no twist. The airplane has a very pronounced -10° anhedral. An all-flying stabilator is placed at the top of the airplane’s vertical fin, creating a “T-tail” configuration.
Lockheed F-104A-1-LO Starfighter 55-2969 (U.S. Air Force)
The F-104A had an empty weight of 13,184 pounds (5,980.2 kilograms). The airplane’s gross weight varied from 19,600 pounds to 25,300 pounds, depending on the load of missiles and/or external fuel tanks.
Internal fuel capacity was 896 gallons (3,392 liters). With Sidewinder missiles, the F-104A could carry two external fuel tanks on underwing pylons, for an additional 400 gallons (1,514 liters). If no missiles were carried, two more tanks could be attached to the wing tips, adding another 330 gallons (1,249 liters) of fuel.
Lockheed F-104A Starfighter three-view illustration with dimensions.
The F-104A was powered by a single General Electric J79-GE-3A engine, a single-spool axial-flow afterburning turbojet, which used a 17-stage compressor and 3-stage turbine. The J79-GE-3A is rated at 9,600 pounds of thrust (42.70 kilonewtons), and 15,000 pounds (66.72 kilonewtons) with afterburner. The engine is 17 feet, 3.5 inches (5.271 meters) long, 3 feet, 2.3 inches (0.973 meters) in diameter, and weighs 3,325 pounds (1,508 kilograms).
55-2969 in General Electric colors. (Pinterest)
The F-104A had a maximum speed of 1,037 miles per hour (1,669 kilometers per hour) at 50,000 feet (15,240 meters). Its stall speed was 198 miles per hour (319 kilometers per hour). The Starfighter’s initial rate of climb was 60,395 feet per minute (306.8 meters per second). The combat ceiling was 55,200 feet (16,825 meters) and the service ceiling was 64,795 feet (19,750 meters).
Armament was one General Electric M61 Vulcan six-barreled revolving cannon with 725 rounds of 20 mm ammunition. An AIM-9B Sidewinder heat-seeking air-to-air missile could be carried on each wing tip, or a jettisonable fuel tank with a capacity of 141.5 gallons (535.6 liters).
Lockheed built 153 of the F-104A Starfighter initial production version. A total of 2,578 F-104s of all variants were produced by Lockheed and its licensees, Canadair, Fiat, Fokker, MBB, Messerschmitt, Mitsubishi and SABCA. By 1969, the F-104A had been retired from service. The last Starfighter, an Aeritalia-built F-104S ASA/M of the Aeronautica Militare Italiana, was retired in October 2004.
55-2969 was one of the original pre-production Lockheed YF-104As, completed 20 August 1956. It was modified to the F-104A standard configuration and assigned to the 83rd Fighter Interceptor Squadron at Hamilton Air Force Base, near Novato, California.
On 22 August 1957 the Starfighter was damaged at Eglin Air Force Base, Florida. It was returned to Lockheed for repair and upgraded to F-104A-1. In May 1958, -969 and another Starfighter were sent to Edwards to attempt setting several speed and altitude records. They were both then returned to the 83rd FIS.
Lockheed F-104A-1-LO Starfighter 55-2969 with a General Electric J79 turbojet engine, circa 1960. (General Electric)
From August 1958 to August 1961, -969 was loaned to General Electric to test improvements to the J79 turbojet engine. While there, it was given the name Queenie, which was painted on the nose along with three playing cards.
In 1964 55-2969 was again returned to Lockheed for conversion to a QF-104A remote-controlled target drone. It was damaged by a AIM-9 Sidewinder missile on 28 September 1968, but was recovered, repaired and returned to service. On its 25th drone mission, 26 January 1971, Queenie was shot down by an experimental XAIM-4H Falcon air-to-air missile fired by an F-4E Phantom II.
Lockheed QF-104A 55-2969 at Eglin Air Force Base circa 1969
¹ FAI Record File Number 9063
² The Speed of Sound at 40,000 feet is 659.8 miles per hour (1,062 kilometers per hour). Captain Irvin’s record average speed was Mach 2.13.
Captain Albert Francis Hegenberger, Air Corps, United States Army. (NASM)
9 May 1932: At McCook Field, Ohio, Captain Albert Francis Hegenberger, Air Corps, United States Army, flew the very first solo instrument approach and landing, using a system which he had developed. The Hegenberger system, which was adopted by both civil and military aviation authorities, used a series of non-directional radio beacons (NDB) and marker beacons on the ground, along with a radio-compass and other gyroscopic instruments and radio receivers aboard the aircraft, a Consolidated NY-2 biplane.
Hegenberger had located one NDB 1,500 feet (457 meters) from the airfield boundary, and another at 1½ miles (2.4 kilometers). They were aligned with the runway centerline. Both had marker beacons which would signal that the airplane was directly overhead. The radio compass aboard the airplane would indicate the direction of the NDB relative to the airplane and lights would illuminate when it passed over the marker beacons. When the airplane was heading directly toward the NDB, the needle pointed to zero.
A Consolidated NY-2 in flight. A hood covers the rear cockpit, preventing the pilot from seeing outside. (San Diego Air and Space Museum)
Captain Hegenberger turned toward the inner NDB from a distance of 50 miles (80 kilometers). He passed over it at a pre-planned altitude. When the lights on the instrument panel came on indicating that he was directly over the inner marker beacon, he turned toward the outer NDB. Crossing the outer marker, Hegenberger made a 180° turn back toward the inner NDB and began his descent. As he passed over the inner NDB again, he reduced engine power and placed the airplane in a landing attitude and waited for it to touch down on the runway.
This flight was the first solo blind instrument flight, approach and landing. (Lt. James H. Doolittle had made a blind instrument flight in 1929, but he carried a safety pilot aboard.) For his accomplishment, Captain Hegenberger was awarded an oak leaf cluster (a second award) for his Distinguished Flying Cross, and received the Collier Trophy, an annual award for the greatest achievement in aeronautics in America.
Captain Albert F. Hegenberger, Air Corps, United States Army, was presented the Collier Trophy by President Franklin D. Roosevelt, 22 July 1935.
Within one week, the Civil Aeronautics Board created a new pilot rating and required that all commercial pilots demonstrate proficiency in instrument flight. In 1935, the CAB adopted Hegenberger’s system and ordered equipment installed at all major airports between New York and Los Angeles.
The Air Corps Newsletter reported the event:
FIRST SOLO BLIND FLIGHT A SUCCESS
By Lieut. Joseph S. Edgerton, Air Reserve.
ANOTHER milestone in aviation progress was reached a few days ago when Capt. Albert F. Hegenberger, Army Air Corps, made the first “blind” solo flight, seeing nothing but the instruments before him from take-off to landing. If the elements which made Hegenberger’s achievement possible can be applied to air transport operations, one of the greatest foes of aviation can be whipped.
Dense ground fog on an air transport today brings all flying to a halt. As long as the fog holds no mail or passengers move by air. The only solution is artificial fog dispersion or “blind landings” through the fog. Fog dispersion so far is impracticable, if not impossible. Blind landings, apparently, form the practicable solution.
Until Captain Hegenberger’s solo flight, no man had landed “blind” and alone though “Jimmy” Doolittle three years ¹ ago landed blind with a check pilot aboard to take over the controls in case Doolittle’s skill failed or his calculations went awry.
Hegenberger used radio to guide him into the field, to mark for him the point at which to begin his glide and to warn him when he neared the field boundary. He employed a super-sensitive altimeter to indicate his altitude above the landing area. Other flight instruments were normal, including artificial horizon, gyro compass, radio compass and standard flight instruments. The flight was made at Dayton, Ohio, home of the Air Corps Materiel Division, where Captain Hegenberger is stationed as navigation officer.
Modest to a fault, quiet and unassuming, Captain Hegenberger is a brilliant figure in aviation, though seldom in the limelight. he first came to public fame when he flew from California to Hawaii with Lieut. Lester Maitland, ² the first Pacific flight. He is regarded as one of the world’s three foremost aerial navigators.
So retiring is Hegenberger that the world remained for many days in the dark as to his achievement. Captain Hegenberger was on the high seas, enroute to Rome to attend the first international meeting of ocean flyers when the story of his success was given to the world by F. Trubee Davision, Assistant Secretary of War for Aeronautics, who learned of the flight from Hegenberger’s official report.
Of the crucial moment when Captain Hegenberger, alone in his swiftly moving plane, felt his way toward the surface of the earth which he could not see, he has little to say in his report. It is difficult for the layman to put himself in Hegenberger’s position during that moment. To get something of the idea, imagine yourself driving in an automobile. The windows are all curtained so that you can get no glimpse of anything outside the car, no sky, no road – nothing but the blank curtains and the instruments. You have a radio direction finder, with a little arrow showing when you deviate to the right or left of a given course. You are driving at 50 miles an hour across an open field. At the far side of the field is a great yawning chasm of appropriate depth – say something like the Grand Canyon. There is but one avenue of safety, a very narrow bridge. If you miss the bridge, curtains. A radio beacon is guiding you to the bridge and your only indication is the little pointer. You may not slacken speed but you must hit the bridge precisely.
Your problem, however, would be much simpler than Hegenberger’s. Gravity would hold you on the ground and you wouldn’t have to worry about that. You would have to worry only about whether you were too far to the left or right. Hegenberger had to worry, not only about whether he was to the right or left of the runway, but also whether he was too high or too low and whether he was actually over the landing field or over some other place or terrain not at all suitable for the landing of airplanes.
It must have been with a feeling of exquisite relief that he felt the wheels touch the ground and the plane roll to a stop safely. Of this feature of the experiment, however Capt. Hegenberger has only this to say: “The radio transmitters mark the field boundary and all you have to do is just fly along the ground, take things gently and easily, and when you feel it hit – well, just ease back on the stick.”
A magnificent flight, and one worthy of a large and imposing monument on the green fields of aeronautical progress. – Washington STAR
Ed. Note:
According to the announcement of Mr. Davidson regarding this first solo Blind Flight, Captain Hegenberger took off and, after flying for five minutes, landed solely by the air of the instruments on the panel in front of him without once seeing outside of the cockpit. This successful flight was the seventh in a series of nine attempts. During the first three flights, observers were carried in the plane who knew nothing of flying. On the seventh flight, Capt. Hegenberger took off alone, made two 180-degree turns and landed at the take-off point. He was guided during this flight by the various instruments already enumerated. One the ground were three radio sets, two of which were of obsolescent type. The cockpit occupied by Captain Hegenberger had a shielded cover which cut off all view outside the plane. He first tuned in on a transmitter distant from the field to simulate cross-country flying. After executing the first 180-degree turn, he tuned in first on a portable transmitter placed 1,000 feet from the border of the field and then on another a mile and a half away. Although flying away from the field he was able by lining up the two radio transmitters to ascertain the correct flight path on which to return for his landing. Executing his second 180-degree turn at a height of 1,000 feet, he began gliding down as he headed for the mile-and-a half station.
Captain Hegenberger explained that for regular blind landings certain refinements of equipment will be needed. He expressed the desire to start a graduate class of Air Corps officers for training in blind flight take-offs and landings. This Army pilot of Hawaiian Flight fame is now on duty as navigation officer at the Materiel Division, Wright Field, Dayton, Ohio. His blind flying experiments are a continuation of those carried out under the Daniel Guggenheim Fund for the Promotion of Aeronautics by former Lieut. James H. Doolittle, now a Major in the Air Corps Reserve, and as brilliant a figure in commercial aviation as he was while actively connected with the Air Corps. On September 24, 1929, Major Doolittle first demonstrated to the world the possibility of landing an airplane by instruments alone. He carried a check pilot to take over the controls in case of emergency.
It may be stated that Captain Hegenberger is a pioneer in blind flying, for nearly nine years ago, on September 6, 1923, he flew the greater part of the journey from Dayton to Boston completely out of sight of land. Of course, there were no hooded cockpits in those days but, so far as vision of the ground was concerned, Captain Hegenberger and his passenger, Mr. Bradley Jones, Navigation Engineer at McCook Field, were not much better off that the present day airman piloting a covered wagon, aerial type.
Despite unfavorable weather conditions, they took off from McCook Field in a DeH at ten o’clock and landed at Boston Airport 7 hours and 25 minutes later. The sky was obscured by clouds which stretched from 300 to 7,000 feet altitude. After sighting Ohio State Univeriity at Columbus, the clouds became so dense that the flyers climbed above them and found themselves in clear sunlight little above 10,000 feet. A solid layer of clouds stretched beneath them. Not a glimpse of a land mark was obtained for a number of hours. The entire State of Pennsylvania was passed over without their obtaining a glimpse of it. Flying by instruments alone, Captain Hegenberger, at about 3:40 p.m., estimated that he should be close to the Hudson River, so he descended through the clouds and crossed this body of water not five minutes later. The remainder of the journey to Boston was made under the clouds. The successful termination of this flight demonstrated the efficiency of air navigation instruments even in those early days of Army aviation.
—Air Corps News Letter, Vol. XVI, No. 6, 26 May 1932, at pages 207–208
1st Lieutenant Albert Francis Hegenberger, Air Service, United States Army, circa 1920–1925. (George Grantham Bain Collection, Library of Congress, Call Number LC-B2-5469-15)
Albert Francis Hegenberger was born 30 September 1895 at Boston, Massachusetts, United States of America. He was the second of five children of Alphonse Frederick Hegenberger, a clerk and immigrant from Bavaria, and Emma Amanda Buegler Hegenberger, of Switzerland.
In 1913 Hegenberger entered the Massachusetts Institute of Technology (M.I.T.), Cambridge, Massachusetts, as a student of aeronautical engineering.
Following the United States’ entry into World War I, Albert F. Hegenberger enlisted as a private in the Aviation Section, Signal Corps, United States Army, 14 September 1917. He was assigned to the School of Military Aeronautics at M.I.T., graduating in December 1917. After flight training at Ellington Field, Houston, Texas, Hegenberger was commissioned a second lieutenant, Aviation Section, Signal Officers Reserve Corps, 6 April 1918. This commission was vacated 19 September 1920, and he was appointed a second lieutenant, Air Service, retroactive to 20 July 1920. He was promoted to the rank of first lieutenant, effective that that same date.
In October 1918, Second Lieutenant Hegenberger returned to M.I.T., and entered the School of Aeronautical Engineering. He graduated in February 1919.
Lieutenant Hegenberger married Miss Louise B. Berchtold in 1919. They would have two sons, Albert F., Jr., born in 1920, and Robert F., born in 1924.
In October 1923, 1st Lieutenant Hegenberger was assigned to the 72nd Bombardment Squadron, 5th Composite Squadron, at Luke Field on the Island of Oahu, Territory of Hawaii. The squadron was equipped with the DH-4 and the twin-engine Martin NBS-1 bomber. In March 1925, Lieutenant Hegenberger was transferred to the 23rd Bombardment Squadron, 5th Composite Group.
Lieutenant Hegenberger was next assigned as chief of the Equipment Branch, Material Division, at McCook Field, Dayton Ohio. He served in that position from October 1926 until June 1927, when became chief of the Instrument and Navigation Unit.
At 7:09 a.m., Pacific Daylight Time, 28 June 1927, 1st Lieutenant Lester J. Maitland and 1st Lieutenant Albert F. Hegenberger, Air Service, United States Army, took off from Oakland Municipal Airport, California, aboard an Atlantic-Fokker C-2, serial number A.S. 26-202, Bird of Paradise. Their destination was Wheeler Field, Honolulu, Territory of Hawaii, 2,407 miles (3,874 kilometers) across the Pacific Ocean.
“Bird of Paradise”, Atlantic-Fokker C-2 serial number 26-202, arrives at Wheeler Field, Honolulu, Territory of Hawaii after a non-stop flight from Oakland, California, 6:29 a.m., 29 June 1927. (U.S. Air Force)
After 25 hours, 50 minutes of flight, Bird of Paradise landed at Wheeler Field, 6:29 a.m., local time, 29 June 1927. It had completed the first Transpacific Flight.
For their achievement, both officers were awarded the Distinguished Flying Cross. They were also awarded the Mackay Trophy for the most meritorious flight of the year.
Secretary of War George Henry Dern presents Captain Albert F. Hegenberger the Distinguished Flying Cross, 18 May 1934. (Harris & Ewing)
1st Lieutenant Hegenberger continued in his technical assignments at McCook and Wright Fields. On 3 January 1932, he was promoted to the rank of captain.
Mrs. Hegenberger died 7 August 1933.
In August 1935, Captain Hegenberger was assigned to the 30th Bombardment Squadron at Rockwell Field, San Diego, California. The squadron moved to March Field, near Riverside, California, and transitioned to the Martin B-10. Captain Hegenberger was advanced to the rank of major (temporary), 2 October 1935.
On 22 July 1937, Major Hegenberger married Ms. Jewel Lilly Van Houten (née Jewel Lilly Baker) at Detroit, Michigan.
From August 1937 to June 1939, Major Hegenberger was assigned to the Air Corps Tactical School, Maxwell Field, Montgomery, Alabama. Upon graduation, he was assigned to the 5th Bombardment Group at Hickam Field, Honolulu, Territory of Hawaii. The 5th was equipped with Keystone B-3 and B-4 bombers.
Major Hegenberger was appointed operations officer of the 18th Wing at Hickam, and then in November 1940, became assistant chief of staff for operations of the Hawaiian Air Force, headquartered at Fort Shafter, near Honolulu. Hegenberger was promoted to lieutenant colonel (temporary), on 30 December 1940. This rank became permanent 18 December 1941.
In April 1941, Lieutenant Colonel Hegenberger took command of the 11th Bombardment Group. The group was equipped with Douglas B-18 Bolo, but began receiving Boeing B-17 Flying Fortresses the following month.
Hegenberger was promoted to colonel (temporary), 5 January 1942. He took command of 18th Bombardment Group and Seventh Bomber Command. He was appointed Colonel, Army of the United States (A.U.S.), 8 June 1942. Returning to the continental United States, Colonel Hegenberger became assistant chief of staff for operations, Second Air Force, and commanding officer, II Bomber Command, at Fort George Wright, Spokane, Washington. In October 1942, Colonel Hegenberger took command of the 21st Bombardment Wing, based at Smoky Hill Army Air Field, Salina, Kansas, and later, Topeka Army Air Field, Topeka, Kansas.
Colonel Hegenberger was promoted to the rank of brigadier general, A.U.S., 18 September 1943. In January 1944, he was appointed Chief of Staff, Second Air Force, at Colorado Springs Army Air Field, Colorado Springs, Colorado.
The following year, January 1945, Brigadier General Hegenberger became Chief of Staff, Fourteenth Air Force, based at Chunking, China.
“Major General C. J. Chow, Director of the Commission on Aeronautical Affairs in Chungking, China, and Brig. General Albert F. Hegenberger, Chief of Staff of the 14th Air Force.” (U.S. Embassy and Consulates in China)
Hegenberger became commanding general, Tenth Air Force, also based in China, in August 1945. He was promoted to major general, A.U.S., 7 September 1945. From December 1945 to July 1946, Major General Hegenberger served at Headquarters Army Air Forces. He was then assigned to Pacific Air Command, United States Army (PACUSA), in Japan. He assumed command of the 1st Air Division, Kadena Army Air Base, Okinawa, in July 1946.
In December 1947, Hegenberger was assigned to the Weapons Group, Headquarters, U.S. Air Force. He then served on the staff of the Assistant Deputy Chief of Staff, Operations, for Atomic Energy. On 19 February 1948, Hegenberger’s previous rank of brigadier general, United States Air Force, became permanent, with date of rank retroactive to 19 September 1943. (He continued in the temporary rank of major general.)
Major General Hegenberger retired from the U.S. Air Force on 31 August 1949 after nearly 32 years of military service. During his career, he was awarded the Distinguished Service Medal, Legion of Merit, Distinguished Flying Cross with one oak leaf cluster (two awards), World War I Victory Medal, American Defense Service Medal, American Campaign Medal, World War II Victory Medal, Asiatic-Pacific Campaign Medal; Order of the Cloud and Banner (Republic of China); and Grande Ufficiale dell’Ordine della Corona d’Italia (Grand Officer, Order of the Crown of Italy).
Major General Albert Francis Hegenberger, United States Air Force (Retired) died at Goldenrod, Florida, 31 August 1983, at the age 87 years. He was buried at All Faiths Memorial Park, Casselbury, Florida.
¹ 24 September 1929. The check pilot was Lieutenant Benjamin Scovill Kelsey. Please see TDiA at: https://www.thisdayinaviation.com/24-september-1929/
² 28–29 June 1927. Please see TDiA at: https://www.thisdayinaviation.com/28-29-june-19/
Major Howard C. Johnson, U.S. Air Force, prepares for his record flight, with Lockheed test pilots Willam M. (“Bill”) Park (center) and Jack Holliman. F-104A Starfighter 55-2957 is in the background. (Lockheed Martin)
7 May 1958: Major Howard Carrol Johnson, United States Air Force, the operations officer of the 83rd Fighter Interceptor Squadron, 78th Fighter Group, based at Hamilton Air Force Base, California, zoom-climbed a Lockheed F-104A Starfighter, serial number 55-2957, to an altitude of 91,243 feet (27,811 meters) over Edwards Air Force Base, establishing a new Fédération Aéronautique Internationale (FAI) altitude record. ¹ The flight was certified by Charles S. Lodgson of the National Aeronautic Association.
Major Howard C. Johnson seated in the cockpit of a Lockheed F-104 Starfighter. (Johnson Family Collection)Major Howard C. Johnson, U.S. Air Force, after his record-setting flight. (U.S. Air Force)
Using techniques developed by Lockheed aerodynamicists, Major Johnson climbed to 41,000 feet (12,497 meters) and accelerated to the Starfighter’s maximum speed in level flight. He then started to climb, maintaining a steady 2.5 G load, until he reached the optimum climb angle. A piece of masking tape applied to the side of the cockpit canopy at the predetermined angle gave Johnson a visual reference during his climb. At approximately 77,000 feet (23,470 meters) the F-104’s J79 turbojet engine had to be shut down to prevent overheating in the thin high-altitude atmosphere. The interceptor continued from that point on a ballistic trajectory until it reached the peak altitude. On the descent, the engine was restarted and Johnson flew the Starfighter back to Edwards Air Force Base.
Major Johnson had broken the altitude record set just 17 days earlier by Lieutenant Commander George C. Watkins, U.S. Navy, flying an experimental Grumman F11F-1F Tiger. The Lockheed F-104 beat the Grumman F11F by 4,362 meters (14,311 feet). ²
Lockheed F-104A Starfighter 55-2957.
The Daily Independent Journal reported:
Hamilton Jet Pilot Sets World Altitude Record
A 37-year-old Novato father of two today holds the world altitude record for flight in a powered aircraft.
Maj. Howard C. Johnson of the 83rd Fighter-Interceptor Squadron at Hamilton Air Force Base yesterday nosed a jet-powered F104 Starfighter to an altitude of 91,249 feet above the Mojave desert.
His mark eclipsed by 2.1 miles an unofficial record of 80,190 feet claimed last Friday by a French Trident 06 at Istres, France.
Major Johnson, operations officer of the 83rd FIS, first Starfighter-equipped unit of the Air Force, took off at 9:40 a.m. from the Palmdale (Los Angeles County) facility of the Lockheed Aircraft Corp., manufacturer of the plane.
He sent the missile-like Starfighter upward on a 55-to-60 degree angle as it swept over the heavily instrumented range at Edwards Air Force Base. Then he pulled up sharply into a high angle climb, and zoomed out into the thin atmosphere over the desert—more than 17 miles above sea level.
Just 27 minutes later, he touched down again at Palmdale.
Describing the flight at a Los Angeles news conference today, the curly-haired major said he flew at 35,000 feet to Santa Barbara, went into a climbing turn at 40,000 feet and gave the jet full power about 10 miles from Mojave. Over Mojave, he went into his climb.
He said he had no trouble controlling the plane. With colder air, he thought, he could have gone higher. The temperature outside the plane at the peak of his climb was minus 43 degrees Fahrenheit. Inside it was 70 degrees above zero.
In the past week he had made six practice flights prior to yesterday’s record breaker.
What does the sky look like at such altitudes?”
I was so busy on most of my flights I didn’t notice,” he said. “On one flight I did and it was sort of a dark purple.”
Johnson estimated he was at his maximum altitude 10 to 15 seconds and was going 622 miles per hour at the top of his climb.
Johnson said he didn’t “feel like I was in outer space.”
“But this obviously is a transition from the atmosphere is a transition from the atmosphere we have known,” he said. “We are on the threshold of space—a step up the ladder.”
Back in Novato, his wife, Doris Jean, was at home at 1260 Cambridge street. Their children, Theodore 10, and Carol, 4, were at school.
Mrs. Johnson knew her husband was out after the record, but she wasn’t worrying, she said today.
“We’ve been married for 16 years and all of that time he has been in the Air Force,” she said, “so I’ve learned not to worry too much.
“He had oxygen and a suit to protect him. But I do wish he’d stay a little lower.”
Mrs. Johnson’s telephone rang soon after 10 o’clock. It was her husband, calling to say he had been successful in setting a new altitude record.”
That’s about all he said,” reported Mrs. Johnson.
The record is subject to review by the Federation Aeronautique Internationale before it goes down in the books as official.
Plane altitude records have been zooming since the adoption of the jet engine. The altitude record for a propeller-drive plane is 56,046 feet, set ‘way back in 1946 by Maj. F. F. Ross, pilot, and Lt. D. M. Davis, flying from Harmon Field on Guam.
An experimental rocket plane has gone higher than Johnson’s Starfighter, but the feats are not comparable. The rocket craft was launched from a mother plane high in the air, while the Starfighter took off from the ground.
A balloon piloted by Maj. David G. Simons ascended to approximately 100,000 feet last Aug. 19 and 20, according to the World Almanac.
Major Johnson is a native of Knoxville, Tenn. He has been in the Air Force since April 1, 1942, and has logged 4,600 hours flying time, including 1,800 hours in jets. He has been stationed in California, at Castle Air Force Base, Merced, and then at Hamilton, for five years.
Lieutenant Colonel Johnson was part of a group of engineers and pilots awarded the Robert J. Collier Trophy by the National Aeronautic Association in 1958 for “the greatest achievement in aeronautics” because of their involvement in the Lockheed F-104 program.
Vice President Richard M. Nixon presents the Collier Trophy. Left to right, Major Walter W. Irwin and Lieutenant Colonel Howard C. Johnson; Nixon; Neil Burgess and Gerhard Neumann, designers of the General Electric J79 engine; and Clarence Leonard (“Kelly”) Johnson, Lockheed Aircraft Corporation. 15 December 1959. (NASM-00142388)Colonel Howard C. Johnson, United States Air Force.
Howard Carrol Johnson was born at Knoxville, Kentucky, 2 February 1920. He was the son of Roscoe Howard Johnson, a railroad clerk, and Clara B. Coker Johnson. When he got into a fight at age 13, he was given the nickname, “Scrappy.” He attended DuPont Manual Training High School in Louisville, and later studied at the University of Louisville.
Johnson registered for Selective Service (conscription), 1 July 1941, in Louisville, Kentucky. He was described as having a light brown complexion, with black hair and brown eyes. He was 5 feet, 8 inches (172.7 centimeters) tall, and weighed 140 pounds (63.5 kilograms). He was employed as a messenger by the L & N Railway in Louisville.
Soon after the United States entered World War II, on 1 April 1942, Johnson enlisted as a private in the Air Corps, United States Army, at Lexington, Kentucky. He was accepted as an aviation cadet 7 April 1942.
He trained at the Harman Flying School, Bollinger, Texas, and at Moore Field, Texas, as a member of Class 43C.
Donna Holder
Aviation Cadet Johnson married Miss Donna Jean Holder, a classmate at the University of Louisville, at the Presbyterian Church, McAllen, Texas, 4:30 p.m., February 20, 1943. They would have two children. Mrs. Johnson died in 1986.
After completing flight training, Aviation Cadet Johnson was commissioned as a second lieutenant, Army of the United States (A.U.S.), 20 March 1943. He was promoted to 1st Lieutenant 27 June 1944.
Lieutenant Johnson was assigned as a gunnery instructor and gunnery target pilot at Laredo Army Airfield, Texas. He flew the North American Aviation AT-6 Texan, Beech AT-11 and Lockheed AT-18 Hudson.
Lieutenant Johnson was promoted to the rank of captain, air reserve (inactive) on 13 November 1946. He was released from active duty 12 January 1947, but maintained his commission as a reserve officer. On 19 June 1947, Johnson’s permanent rank reverted to first lieutenant, Air Corps, with a date of rank of 20 March 1946.
Johnson returned to active duty 28 August 1947.
During the Korean War, Captain Johnson flew 87 combat missions in the North American Aviation F-51 Mustang. From 1952 to 1953, Captain Johnson was assigned to Goose Bay Air Base, Newfoundland and Labrador, Canada. He flew the Lockheed F-94B a two-place radar-equipped interceptor on interception missions over the Arctic. He then served with the 83rd and 84th Fighter-Interceptor Squadrons at Hamilton Air Force Base, California, 1954-1955.
From 1958 to 1960 Major Johnson was assigned to the North American Air Defense Command (NORAD) at Colorado Springs, Colorado.
During the Berlin crisis of 1961, Major Johnson was deployed to West Germany, flying the Republic F-84F Thunderstreak. He served as an advisor to the West German Air Force.
Major Johnson commanded the 476th Tactical Fighter Squadron at George Air Force Base, California, 1963–1964, and the 476th TFS, 1964–1965. From 1966 to 1967, Johnson was assigned to the 388th Tactical Fighter Wing at Korat Royal Thai Air Force Base, Thailand, as Director of Operations. He flew 117 combat missions in the Republic F-105 Thunderchief over Southeast Asia. He was a founding member of the Red River Valley Pilot’s Association.
Colonel Johnson retired from the Air Force 1 October 1972 after 30 years of service. He bought a cattle ranch near Lake Texoma, Texas. He later a owned live-aboard boat, Scalawag, home-ported at Palm Beach, Florida.
Johnson married Ms. Elena Amelia Rova O’Brien, a widow, 17 April 1990, at West Palm Beach, Florida. Mrs. Johnson died in 2016.
Johnson next married Kathryn Theresa O’Brien, 30 years his junior, in Palm Beach, Florida, 5 July 2018.
Colonel Johnson died 9 December 2020 at the age of 100 years. He was buried at the Memorial Park Cemetery, New Iberia, Louisiana.
During his career in the United States Air Force, Colonel Johnson was awarded the Silver Star (two awards); the Legion of Merit (two awards); the Distinguished Flying Cross (seven awards); and the Air Medal (18 awards).
The landing gear are retracting as Major Howard C. Johnson takes off with the Lockheed F-104A Starfighter, 55-2957, 7 May 1958. (U.S. Air Force)
The Lockheed F-104A Starfighter was a single-place, single engine supersonic interceptor. It was designed by a team lead by the legendary Clarence L. “Kelly” Johnson.
The F-104A is 54.77 feet (16.694 meters) long with a wingspan of 21.94 feet (6.687 meters) and overall height of 13.49 feet (4.112 meters). The total wing area is just 196.1 square feet (18.2 square meters). At 25% chord, the wings are swept aft 18° 6′. They have 0° angle of incidence and no twist. The airplane has a very pronounced -10° anhedral. An all-flying stabilator is placed at the top of the airplane’s vertical fin, creating a “T-tail” configuration.
The F-104A had an empty weight of 13,184 pounds (5,980.2 kilograms). The airplane’s gross weight varied from 19,600 pounds to 25,300 pounds, depending on the load of missiles and/or external fuel tanks.
Internal fuel capacity was 896 gallons (3,392 liters). With Sidewinder missiles, the F-104A could carry two external fuel tanks on underwing pylons, for an additional 400 gallons (1,514 liters). If no missiles were carried, two more tanks could be attached to the wing tips, adding another 330 gallons (1,249 liters) of fuel.
Lockheed F-104A Starfighter three-view illustration with dimensions.
The F-104A was powered by a single General Electric J79-GE-3A engine, a single-spool axial-flow afterburning turbojet, which used a 17-stage compressor and 3-stage turbine. The J79-GE-3A is rated at 9,600 pounds of thrust (42.70 kilonewtons), and 15,000 pounds (66.72 kilonewtons) with afterburner. The engine is 17 feet, 3.5 inches (5.271 meters) long, 3 feet, 2.3 inches (0.973 meters) in diameter, and weighs 3,325 pounds (1,508 kilograms).
The F-104A had a maximum speed of 1,037 miles per hour (1,669 kilometers per hour) at 50,000 feet (15,240 meters). Its stall speed was 198 miles per hour (319 kilometers per hour). The Starfighter’s initial rate of climb was 60,395 feet per minute (306.8 meters per second) and its service ceiling was 64,795 feet (19,750 meters).
Armament was one General Electric M61 Vulcan six-barreled revolving cannon with 725 rounds of 20 mm ammunition. An AIM-9B Sidewinder heat-seeking air-to-air missile could be carried on each wing tip, or a jettisonable fuel tank with a capacity of 141.5 gallons (535.6 liters).
The Lockheed F-104 was armed with an electrically-powered General Electric T-171E-3 (later designated M61) Vulcan 6-barrel rotary cannon, or “Gatling Gun.” The technician has a belt of linked 20 mm cannon shells. (SDASM)
Lockheed built 153 of the F-104A Starfighter initial production version. A total of 2,578 F-104s of all variants were produced by Lockheed and its licensees, Canadair, Fiat, Fokker, MBB, Messerschmitt, Mitsubishi and SABCA. By 1969, the F-104A had been retired from service. The last Starfighter, an Aeritalia-built F-104S ASA/M of the Aeronautica Militare Italiana, was retired in October 2004.
55-2957 had been one of the first group of YF-104A pre-production aircraft. After the flight test program, it and the others were modified to the F-104A production standard.
The record-setting Lockheed F-104A Starfighter was later converted to a QF-104A high-speed drone. It was expended as a target 8 August 1967.
Lockheed QF-104A Starfighter 55-2957 in flight after modification to high-speed drone configuration. There is no pilot aboard. (U.S. Air Force)
Lockheed XC-35 36-353 in flight. (U.S. Air Force)Headle
1 May 1937: The Lockheed Aircraft Company’s chief test pilot, Marshall Headle, took the Lockheed XC-35, Air Corps serial number 36-353, for its first flight. Ordered by the Air Corps in 1936 as a high-altitude research aircraft, and for the development of cabin pressurization, the XC-35 Supercharged Cabin Transport Airplane was a highly modified Lockheed Electra 10A. It was the first airplane to be specifically built with a pressurized cabin.
The Citizen-News, Hollywood, California, reported:
Mystery Airplane In Air For Tests
The Army’s secretly built stratosphere plane took off on its first test flight today at the Lockheed Aircraft Corp’s factory at Burbank with Marshall Headle, chief test pilot for the company, its sole occupant.
Only routine, low altitude maneuvers were to be carried out today, however, to test the plane’s flying characteristics, and it was expected that high altitude tests would not begin until next week.
Shortly before noon a canvas curtain that was erected about the mystery plane immediately after an unauthorized photograph brought stormy protests from the War Dept., was lowered and the big twin engined, low wing craft rumbled to the end of the factory airport.
A quick sprint and the silver bodied plane was in the air safely.
Company officials continued their silence on performance expected of the military experimental ship.
The XC-35 had been rolled out of the plant several days earlier. It was photographed by a newspaper photographer and the image published in a local newspaper. The photographer had hidden behind bushes on a small hill near the plant. This resulted in an immediate response from the military, with the airplane being hidden behind a canvas enclosure. Armed guards were ordered to “shoot cameras out of the hands of photographers and ask questions afterward—but to destroy all cameras.” There were also roving vehicle patrols, etc. Army intelligence officers interrogated the photographer.
The Army Air Corps was awarded the Collier Trophy for 1937 for the XC-35 project.
With a strengthened circular fuselage and smaller windows, the XC-35′s passenger compartment was pressurized by engine turbo-superchargers and controlled by a flight engineer. Cabin pressure could be maintained at the equivalent of 12,000 feet (3,658 meters) above sea level, at an actual altitude of 30,000 feet (9,144 meters).
Lockheed XC-35 engineer station. (U.S. Air Force)
A crew of three and two passengers were accommodated within the pressurized section, and there was room for another passenger to the rear of the pressure bulkhead, which could only be used at lower altitudes.
Lockheed XC-35 36-353.
The Lockheed XC-35 was similar to the Lockheed Model 10 Electra, with the same dimensions: length, 38 feet, 7 inches (11.760 meters), wingspan 55 feet (16.764 meters), and height, 10 feet, 1 inch (3.073 meters). It had a total wing area of 458.5 square feet (42.596 square meters). The airplane had an empty weight of 7,940 pounds (3,602 kilograms), and gross weight of 10,500 pounds (4,763 kilograms).
The Lockheed XC-35 was powered by two air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney R-1340-43 (Wasp T5H1) single-row, nine-cylinder radial engines with a compression ratio of 6:1. The R-1340-43 had a Normal and Takeoff Power rating of 550 horsepower at 2,200 r.p.m. from Sea Level to 3,000 feet (914 meters), burning 92-octane gasoline. It was direct drive. The engine was 3 feet, 6.25 inches (1.073 meters) long, 4 feet, 3.50 inches (1.308 meters) in diameter, and weighed 864 pounds (392 kilograms). The engines drove two-bladed, variable pitch propellers.
The XC-35 had a cruise speed of 214 miles per hour (344 kilometers per hour), and maximum speed of 236 miles per hour (380 kilometers per hour) at 20,000 feet (6,096 meters). It could climb at a rate of 1,125 feet per minute (5.7 meters per second), and its service ceiling was 31,500 feet (9,601 meters).
Able to fly above 30,000 feet (9,144 meters), the XC-35 was later used by NACA for thunderstorm penetration research flights. In 1948 it was transferred to the Smithsonian Institution.
