28 May 1935: Bayerische Flugzeugwerke Aktiengesellschaft (BFW) test pilot Hans-Dietrich Knoetzsch took the prototype Bf 109 V1 fighter, civil registration D-IABI, on its first flight at Haunstetten, near Augsburg, Germany. The duration of the flight was twenty minutes.
The new fighter was designed by Wilhelm Emil Messerschmitt, Walter Rethel and Robert Lusser. It was a light weight, single-seat, single-engine, low-wing monoplane with retractable landing gear.
The first prototype, Versuchsflugzeug 1, was 8.884 meters (29.147 feet) long with a wingspan of 9.890 meters (32.448 feet). The empty weight was 1,404 kilograms (3,095 pounds) and the maximum weight was 1,800 kilograms (3,968 pounds).
Because the Junkers Jumo 210 inverted V-12 engines planned for the new fighter were not yet available, a liquid-cooled, supercharged, 1,295.91-cubic-inch-displacement (21.24 liter) Rolls-Royce Kestrel VI single overhead cam (SOHC) 60° V-12 was installed. This British engine had four valves per cylinder and a compression ratio of 6.00:1. It produced 695 horsepower at 2,500 r.p.m., and turned a two-bladed, fixed-pitch Propellerwerk Gustav Schwarz laminated composite propeller through a 0.553:1 gear reduction. The Kestrel was 6 feet, 0.35 inches (1.838 meters) long, 2 feet, 11.00 inches (0.889 meters) high and 2 feet, 0.40 inches (0.620 meters) wide. It weighed 955 pounds (433 kilograms).
V1’s maximum airspeed was 470 kilometers per hour (292 miles per hour) and its maximum altitude was 8,000 meters (26,247 feet).
No armament was installed on the prototype.
The Bf 109 V1 was tested for several months before being sent to the Luftwaffe test center at Rechlin for acceptance trials. The prototype’s landing gear collapsed while landing there.
The prototype Bf 109 was revealed to the public when D-IABI flew at the Games of the XI Olympiad (the 1936 Summer Olympics, held at Berlin, Germany).
The Bf 109 (also known as the Me 109, following Willy Messerschmitt’s acquisition of BFW) was produced from 1937 to 1945. Total production was 33,894 aircraft, which amounted to 57% of total fighter production for Germany. Seven plants produced the Bf 109 during World War II.
After the war ended, Czechoslovakia produced a variant until 1948. Another Spanish-built variant remained in production until 1958.
27 May 1958: At Lambert Field, St. Louis, Missouri, McDonnell Aircraft Corporation’s Chief Test Pilot (and future company president) Robert C. Little made the first flight of the YF4H-1 prototype. The twin-engine Mach 2+ airplane was the first pre-production model of a new U.S. Navy fleet defense interceptor that would be developed into the legendary F-4 Phantom II fighter bomber.
The flight lasted 22 minutes. Little had planned to go supersonic but a leak in a pressurized hydraulic line caused him to leave the landing gear extended as a precaution, should the back-up hydraulic system also have a problem. This limited the maximum speed of the prototype to 370 knots (426 kilometers per hour). A post-flight inspection found foreign-object damage to the starboard engine.
Initially designated XF4H-1 and assigned Bureau of Aeronautics serial number (“Bu. No.”) 142259, the identifier was changed to YF4H-1. It had been in development for over five years based on a company proposal to the Navy.
The McDonnell YF4H-1 Phantom II was 56 feet, 7.9 inches (17.271 meters) long with a wingspan of 38 feet, 4.89 inches (11.707 meters) and overall height of 16 feet, 3.0 inches (4.953 meters). With wings folded, the airplane’s span was narrowed to 27 feet, 6.6 inches (8.397 meters). The wings were swept 45°, measured at 25% chord. The inner wing had no dihedral, while the outer panels had 12° dihedral. The stabilator had a span of 16 feet, 5.0 inches (5.004 meters), with -23.25° anhedral. The wheelbase of Phantom II’s tricycle undercarriage was 23 feet, 3.25 inches (7.093 meters), with a main wheel tread of 17 feet, 10.46 inches (5.447 meters).
The YF4H-1 prototype was powered by two General Electric J79-GE-2 engines. These were single-spool, axial-flow turbojet engines with a 17-stage compressor and 3-stage turbine. The J79-GE-2 was rated at 10,350 pounds of thrust (46.039 kilonewtons), and 16,150 pounds (71.389 kilonewtons) with afterburner. The engines were 17 feet, 4.0 inches (5.283 meters) long, 3 feet, 2.3 inches in diameter (0.973 meters), and each weighed 3,620 pounds (1,642 kilograms).
The production F4H-1 (F-4B) had a maximum speed of 845 miles per hour (1,360 kilometers per hour) at Sea Level and 1,485 miles per hour (2,390 kilometers per hour) at 48,000 feet (14,630 meters meters). (Mach1.11 and Mach 2.25, respectively). The service ceiling was 62,000 feet (18,898 meters) and maximum range with external fuel was 2,300 miles (3,700 kilometers).
The second prototype YF4H-1, Bu. No. 142260, flown by Commander Lawrence E. Flint, Jr., USN, set a Fédération Aéronautique Internationale (FAI) World Record for Altitude, 6 December 1959, when it zoom-climbed to 30,040 meters (98,556 feet).¹ On 22 November 1961, 142260, flown by Lieutenant Colonel Robert B. Robinson, USMC, also set an FAI World Record for Speed over a Straight 15/25 Kilometer Course, averaging 2,585.425 kilometers per hour (1,606.509 miles per hour).² On 5 December 1961, the same Phantom set an FAI World Record for Altitude in Horizontal Flight at 20,252 meters (66,444 feet) with Commander George W. Ellis, USN, in the cockpit.³
The F-4A through F-4D Phantoms were armed with four AIM-7 Sparrow radar-homing air-to-air missiles, and could carry additional Sparrows or AIM-9 Sidewinder infrared-homing missiles on pylons under the wings. Up to 16,000 pounds (7,257 kilograms) of bombs could be carried on five hardpoints.
McDonnell Aircraft built two YF4H-1 prototypes, followed by 45 F4H-1F (F-4A) Phantom IIs before the F-4B was introduced in 1961. 649 F-4Bs were produced. The initial U.S. Air Force variant was the F-110A Spectre (F-4C Phantom II). McDonnell Douglas delivered its last Phantom II, an F-4E-67-MC, on 25 October 1979. In 21 years, the company had built 5,057 Phantom IIs.
After 11 test flights at St. Louis, Bob Little flew the YF4H-1 west to Edwards Air Force Base in California where more detailed flight testing and evaluation took place.
On 21 October 1959, a failure of an engine access door led to a cascading series of problems which resulted in the loss of the airplane and death of the pilot, Gerald “Zeke” Huelsbeck.
Wing Commander Guy Penrose Gibson, DSO and Bar, DFC and Bar, was awarded the Victoria Cross by His Majesty King George VI at a ceremony at RAF Scampton. Wing Commander Gibson received the medal for his leadership of No. 617 Squadron, The Dambusters, during Operation Chastise, the attack on Germany’s Ruhr Valley hydroelectric dams, 16–17 May 1943.
The Victoria Cross ranks with the George Cross as the United Kingdom’s highest award for gallantry.
The first British medal to be created for bravery, the Victoria Cross was instituted in 1856, with the first recipients being personnel honoured for their gallantry during the Crimean War.
The bronze cross pattée, which bears the inscription “FOR VALOUR,” is cast from the metal of Russian guns captured at Sevastopol during the Crimean campaign. The Victoria Cross is awarded “for most conspicuous bravery, or some daring or pre-eminent act of valour or self-sacrifice, or extreme devotion to duty in the presence of the enemy.”
Air Ministry, 28th May, 1943.
ROYAL AIR FORCE.
The KING has been graciously pleased to confer the VICTORIA CROSS on the undermentioned officer in recognition of most conspicuous bravery: —
Acting Wing Commander Guy Penrose GIBSON, D.S.O., D.F.C. (39438), Reserve of Air Force Officers, No. 617 Squadron: —
This officer served as a night bomber pilot at the beginning of the war and quickly established a reputation as an outstanding operational pilot. In addition to taking the fullest possible share in all normal operations, he made single-handed attacks during his “rest” nights on such highly defended objectives as the German battleship Tirpitz, then completing in Wilhelmshaven.
When his tour of operational duty was concluded, he asked for a further operational posting and went to a night-fighter unit instead of being posted for instructional duties. In the course of his second operational tour, he destroyed at least three enemy bombers and contributed much to the raising and development of new night-fighter formations.
After a short period in a training unit, he again volunteered for operational duties and returned to night bombers. Both as an operational pilot and as leader of his squadron, he achieved outstandingly successful results and his personal courage knew no bounds. Berlin, Cologne, Danzig, Gdynia, Genoa, Le Creusot, Milan, Nuremberg and Stuttgart were among the targets he attacked by day and by night.
On the conclusion of his third operational tour, Wing Commander Gibson pressed strongly to be allowed to remain on operations and he was selected to command a squadron then forming for special tasks. Under his inspiring leadership, this squadron has now executed one of the most devastating attacks of the war—the breaching of the Moehne and Eder dams.
The task was fraught with danger and difficulty. Wing Commander Gibson personally made the initial attack on the Moehne dam. Descending to within a few feet of the water and taking the full brunt of the antiaircraft defences, he delivered his attack with great accuracy. Afterwards he circled very low for 30 minutes, drawing the enemy fire on himself in order to leave as free a run as possible to the following aircraft which were attacking the dam in turn.
Wing Commander Gibson then led the remainder of his force to the Eder dam where, with complete disregard for his own safety, he repeated his tactics and once more drew on himself the enemy fire so that the attack could be successfully developed.
Wing Commander Gibson has completed over 170 sorties, involving more than 600 hours operational flying. Throughout his operational career, prolonged exceptionally at his own request, he has shown leadership, determination and valour of the highest order.
—The London Gazette, Tuesday, 25 May 1943, No. 3630 at Page 2361
27 May 1919: NC-4, designating number A2294, one of three United States Navy Curtiss NC flying boats, arrived at the harbor of Lisbon, Portugal, becoming the first airplane to cross the Atlantic Ocean.
NC-4 was under the command of Lieutenant Commander Albert Cushing Read, United States Navy, who also served as navigator. The pilots were First Lieutenant Elmer Fowler Stone, United States Coast Guard, and Lieutenant (j.g.) Walter T. Hinton, U.S. Navy. Lieutenant James L. Breese, USN and Chief Machinist Mate Eugene S. Rhoads, USN, were the engineers. Ensign Herbert C. Rodd, USN, was the radio operator.
Aboard the other aircraft were officers who would rise to high rank in the Navy: Commander John H. Towers would later command the Pacific Fleet; Lieutenant Marc A. Mitscher commanded the Fast Carrier Task Force during World War II, and later commanded the Atlantic Fleet. Lieutenant Patrick N.L. Bellinger commanded Patrol Wing 2 at Pearl Harbor on 7 December 1941, and would go on to command Naval Air Forces, Atlantic Fleet.
Three Curtiss flying boats, NC-1 (A2291), NC-3 (A2293) and NC-4 (A2294), under the command of Lieutenant Commander John H. Towers, USN, departed Naval Air Station Rockaway, New York City, at 10:00 a.m., 8 May 1919 and flew to NAS Chatham, Massachusetts.
Enroute, NC-4 experienced an oil leak from the center pusher engine, so it was shut down. This slowed the airplane, but it was still able to continue. In mid-afternoon, however, the center tractor engine suffered a failed connecting rod. With only two engines operating, NC-4 was forced down at sea, approximately 80 miles (129 kilometers) from Chatham. The sea was calm and the flying boat taxied the remaining distance on the water. It arrived there at 7:00 a.m., 9 May.
At the air station, the failed engine was replaced with a 300 horsepower Liberty L12, the only spare engine available. The other engine was repaired.
Delayed several days by weather, NC-4 departed NAS Chatham at 9:15 a.m., 14 May, and flew to Halifax, Nova Scotia, landing at 1:07 p.m. Continuing to Newfoundland would have them arriving after dark.
NC-4 took off from the waters of Halifax the following morning at 11:47 a.m., and arrived at Trepassey Bay, Newfoundland at 5:41 p.m., rendezvousing with the aircraft tender USS Aroostook (CM-3). NC-1 and NC-3 had arrived two days earlier.
All three airplanes were serviced from the tender. The temporary 300 horsepower Liberty engine which had been installed on NC-4 was replaced with a correct 400 horsepower engine.
The three Curtiss flying boats took off from Trepassey Bay at 6:00 p.m. on the evening of 16 May and headed across the Atlantic Ocean to the Azores.
NC-1 and NC-3 were both forced down by rain, heavy clouds and thick fog about 200 miles short of their destination. NC-1 was damaged and unable to continue. The crew was rescued by a Greek freighter and the airplane taken in tow, but it sank several days later. NC-3 drifted for two days on surface of the Atlantic, coming within sight of land, two engines were started and NC-3 taxied into the harbor at Ponta Delgada, Ilha de São Miguel.
NC-4 deviated from its course and landed at Horta, on Faial Island, at 1:23 p.m., 17 May. Weather kept NC-4 at Horta for the next few days, until at 8:45 a.m. on the 20th, it took off and flew to Ponta Delgado, landing there just two hours later.
Again, NC-4 was forced to remain in harbor waiting for favorable weather. On 27 May, it was good enough to resume the journey, and the crew once again took off, this time enroute to Lisbon, Portugal.
At 8:01 p.m., 27 May 1919, NC-4 touched down on the Tagus Estuary, Lisbon, and became the very first airplane to complete a flight across the Atlantic Ocean.
NC-4 was the fourth of ten NC flying boats built by the Curtiss Aeroplane and Motor Company. It was 68 feet, 3 inches (20.803 meters) long with a wingspan of 126 feet (38.405 meters) and height of 24 feet, 6 inches (7.468 meters). The empty weight was 15,874 pounds (7,200.3 kilograms) and maximum takeoff weight was 21,500 pounds (9,752.2 kilograms).
Originally built with three engines, flight testing led to the addition of a fourth. These were water-cooled, normally-aspirated, 1,649.336-cubic-inch-displacement (27.028 liter) Liberty L-12 single overhead cam (SOHC) 45° V-12 engines with a compression ratio of 5.4:1. The Liberty produced 408 horsepower at 1,800 r.p.m. Two were mounted in a center nacelle with one in tractor and one in pusher configuration. Two more were in individual nacelles in tractor configuration.
NC-4 had a maximum speed of 90 miles per hour (145 kilometers per hour), a service ceiling of 4,500 feet (1,372 meters) and range of 1,470 miles (2,366 kilometers).
NC-4 was restored by the Smithsonian Institution during the early 1960s and remains a part of its collection, though it is on long term loan to the Naval Aviation Museum, Pensacola, Florida.
26 May 1961: The Firefly, the Blériot Trophy-winning Convair B-58A-10-CF Hustler, serial number 59-2451, assigned to the 43rd Bombardment Wing, Carswell Air Force Base, Fort Worth, Texas, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Recognized Course by flying from Washington, D.C. to Paris in 3 hours, 39 minutes, 49 seconds, for an average speed of 1,687.69 kilometers per hour (1,048.68 miles per hour).¹
During the same flight, the B-58 flew the New York to Paris segment in 3 hours, 14 minutes, 44.53 seconds, at an average speed of 1,753.16 kilometers per hour (1,089.36 miles per hour).
The aircrew, Major William R. Payne, Aircraft Commander, Captain William L. Polhemus, Navigator, and Captain Raymond R. Wagener, Defensive Systems Officer, won the Harmon and Mackay Trophies for this flight.
On 3 June 1961, while enroute home, The Firefly crashed only 5 miles from Paris, killing the Blériot Trophy-winning aircrew, Major Elmer E. Murphy, Major Eugene Moses, and First Lieutenant David F. Dickerson. The B-58 was totally destroyed.
The B-58 Hustler was a high-altitude Mach 2 strategic bomber which served with the United States Air Force from 1960 to 1970. It was crewed by a pilot, navigator/bombardier and a defensive systems operator located in individual cockpits. The aircraft is a delta-winged configuration similar to the Convair F-102A Delta Dagger and F-106 Delta Dart supersonic interceptors.
The Hustler is 96 feet, 10 inches (29.515 meters) long, with a wing span of 56 feet, 10 inches (17.323 meters) and an overall height of 31 feet 5 inches (9.576 meters). The wing’s leading edge is swept back at a 60° angle and the fuselage incorporates the “area rule” which resulted in a “wasp waist” or “Coke bottle” shape for a significant reduction in aerodynamic drag. The airplane’s only control surfaces are two “elevons” and a rudder, and there are no flaps.
The B-58A was powered by four General Electric J79-GE-5 axial-flow afterburning turbojet engines, suspended under the wings from pylons. This was a single-shaft engine with a 17-stage compressor and 3-stage turbine, rated at 10,300 pounds of thrust (45.82 kilonewtons), and 15,600 pounds (69.39 kilonewtons) with afterburner. The J79-GE-5 was 16 feet, 10.2 inches (5.136 meters) long and 3 feet, 2.0 inches (0.965 meters) in diameter.
The bomber had a cruise speed of 610 miles per hour (981.7 kilometers per hour) and a maximum speed of 1,325 miles per hour (2,132.4 kilometers per hour). The service ceiling is 64,800 feet (19,751 meters). Unrefueled range is 4,400 miles (7,081 kilometers). Maximum weight is 168,000 pounds (76,203.5 kilograms).
The B-58 weapons load was a combination of W-39, B43 or B61 nuclear bombs. The weapons could be carried in a jettisonable centerline pod, which also carried fuel. The smaller bombs could be carried on underwing hardpoints. There was a defensive 20 mm M61 rotary cannon mounted in the tail, with 1,200 rounds of ammunition and controlled by the Defensive Systems Officer.