Bryan R. Swopes grew up in Southern California in the 1950s–60s, near the center of America's aerospace industry. He has had a life-long interest in aviation and space flight. Bryan is a retired commercial helicopter pilot and flight instructor.
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President John F. Kennedy at Rice University Stadium, Houston, Texas, 12 September 1962. (Cecil Stoughton, White House/John F. Kennedy Library)
“We choose to go to the moon. We choose to go to the moon in this decade and do the other things, not because they are easy, but because they are hard. . . .”
— John Fitzgerald Kennedy, Thirty-Fifth President of the United States of America, in a speech at Rice University, Houston, Texas, 12 September 1962.
And so, 2,500 days later. . .
Apollo 11/Saturn V launches from Pad 39A, Kennedy Space Center, Cape Canaveral, Florida, at 13:32:00.06 UTC, 16 July 1969. Destination: Mare Tranquillitatis, The Moon. (NASA)
The Gloster G.37, prototype of the Gloster Gladiator Mk.I (Gloster Aircraft Co., Ltd.)
12 September 1934: Hawker Aircraft Company test pilot Flying Officer Phillip Edward Gerald Sayer made the first flight of the Gloster G.37, a prototype fighter for the Royal Air Force, designed to reach a speed of 250 miles per hour (402 kilometers per hour) while armed with four machine guns. The flight took place at Gloster’s private airfield at Brockworth, Gloucestershire.
The Gladiator was designed by Gloster’s chief designer, Henry Philip Folland.
The Gladiator was a single-place, single-engine, single-bay biplane, with fixed landing gear. The airplane was primarily of metal construction, though the aft fuselage, wings and control surfaces were fabric covered.
The production Gladiator Mk.I was 27 feet, 5 inches (8.357 meters) long with a wingspan of 32 feet, 3 inches (9.830 meters) and overall height of 11 feet, 9 inches (3.581 meters). It had an empty weight of 3,217 pounds (1,459 kilograms) and gross weight of 4,594 pounds (2,084 kilograms).
Gloster G.37 prototype, right profile
The G.37 was equipped with a left-hand tractor, air-cooled, supercharged, 1,519.083 cubic-inch-displacement (24.893 liters) Bristol Mercury IV-S2 nine cylinder radial engine. With a compression ratio of 5.3:1, the IV-S2 was rated at 505 horsepower at 2,250 r.p.m., and 540 h.p. at 2,600 r.p.m., both at 13,000 feet (3,962 meters). It developed a maximum 560 horsepower at 2,600 r.p.m. at 16,000 feet (4,877 meters). The engine had a take-off power rating of 530 horsepower at 2,250 r.p.m., at Sea Level (3-minute limit). The IV-S2 drove a two-bladed fixed-pitch propeller through a 0.655:1 gear reduction. This engine weighed 920 pounds (417 kilograms).
The G.37 was repowered with a Bristol Mercury VI-S engine, which had a 6:0:1 compression ratio and a 0.5:1 gear reduction ratio. This engine produced a maximum of 636 horsepower at 2,750 r.p.m. at 15,500 feet.
The prototype was armed with two synchronized, air-cooled Vickers .303-caliber machine guns, firing forward through the propeller arc, and two .303-caliber Lewis guns mounted under the bottom wing.
With the upgraded engine and armament, the G.37 reached 242 miles per hour (389 kilometers per hour).
The Gloster Gladiator Mk.I with an enclosed cockpit and a Bristol Mercury IX engine had a maximum speed of 257 miles per hour (414 kilometers) per hour) at 14,600 feet (4,450 meters).
This production Gloster Gladiator Mk.I, K6131, shows the cockpit enclosure. (This airplane, the second production Gladiator Mk.I, was damaged beyond repair when it ran out of fuel near RAF Church Fenton, 26 March 1938.) (Royal Air Force)Gloster Gladiator Mk.I L8032. (SDASM)
The Gladiator Mk.I entered service with the Royal Air Force in February 1937. It was the last biplane fighter to do so, and was the first fighter with an enclosed cockpit. Beginning with No. 72 Squadron, eight fighter squadrons were equipped with the type, though by the beginning of World War II, these were being phased out by more modern airplanes like the Hawker Hurricane and Supermarine Spitfire.
A total of 737 Gloster Gladiators, Mk.I and Mk.II, were built. In addition to the Royal Air Force, there were operated by several other countries in Europe, the Mediterranean and the Middle East.
Prototype Gloster Gladiator G.37 in flight, now marked K5200. A .303-caliber Lewis machine gun is visible under the right wing. (Royal Air Force)Phillip E.G. Sayer, O.B.E. (Flight)
Phillip Edward Gerald Sayer was born at Colchester, England, 2 February 1905. He was the second of three children of Edward James Sayer, a retired British Army officer and Ethel Jane Hellyar Sayer.
Sayer was granted a short service commission in the Royal Air Force as a Pilot Officer on probation, 30 June 1924. His rank was confirmed 23 May 1925. He was promoted to Flying Officer 30 March 1926. Flying Officer Sayer was transferred to the R.A.F. Reserve, 2 March 1929.
In 1930, Gerry Sayer joined Hawker Aircraft Company as a test pilot. When Hawker took over Gloster Aircraft Co., Ltd. in November 1934, he was appointed Chief Test Pilot of Gloster.
Flight Lieutenant Sayer completed his service and relinquished his commission, 2 March 1937. He was permitted to retain his rank.
On 15 May 1941, Sayer made the first flight of the Gloster-Whittle E.28/39, a prototype jet fighter.
Chief Test Pilot Phillip Edward Gerald Sayer, Esq., was appointed an Officer of the Most Excellent Order of the British Empire (OBE) in the New Years Honours list, 30 December 1941.
Gerry Sayer was flying a Hawker Typhoon from RAF Acklington, 22 October 1942, to the Druridge Bay gunnery range. He never returned.
Bell Helicopter Company prototype Model 206L LongRanger, N206L. (Vertical Flight Society)
11 September 1974: The first prototype Model 206L made its first flight at the Bell Helicopter Company plant at Hurst, Texas.
Based on the Bell 206B-3 JetRanger III, the LongRanger featured a 30-inch (76.2 centimeters) stretch to the passenger cabin, a lengthened tail boom and longer main rotor blades. It retained the JetRanger’s Allison 250-C20B turboshaft engine.
¹ As of 11 September 2024, This Day in Aviation has published 1,667 articles.
Pyotr Maksimovich Ostapenko (Encyclopedia of Safety)
11 September 1962: Flying the E-152\1, a record-setting prototype Mikoyan Gurevich interceptor, test pilot Pyotr Maksimovich Ostapenko set a new Fédération Aéronautique Internationale (FAI) World Record for Altitude in Horizontal Flight of 22,670 meters (74,377 feet).¹
Profile of Mikoyan-Gurevich E-152\1 (testpilot.ru)
In documents submitted to FAI, the E-152\1 was identified as E-166. Colonel Georgy Konstantinovich Mosolov made the first flight of the E-152\1 on 21 April 1961. The aircraft displayed at The Central Museum of the Air Forces at Monino, Russia as E-166 is actually the E-152\2, sister ship of the record-setting prototype.
This individual airplane set two other FAI world records. Test Pilot Alexander Vasilievich Fedotov flew it to 2,401 kilometers per hour (1,492 miles per hour) over a 100 kilometer course, 10 October 1961,² and on 7 July 1962, Colonel Mosolov set a world record for speed over a straight 15/25 kilometer course of 2,681 kilometers per hour (1,666 miles per hour).³
The Mikoyan-Gurevich E-152\1 shown with air-to-air missiles and a centerline fuel tank.
The Mikoyan Gurevich E-152\1 is a single-place, single-engine delta-winged prototype all-weather interceptor. It is 19.656 meters (64 feet, 5.4 inches) long with a wingspan of 8.793 meters (28 feet, 10.2 inches). The leading edge of the wings are swept back to 53° 47′. The E-152\1 had an empty weight of 10,900 kilograms (24,030 pounds) and gross weight of 14,350 kilograms (31,636 pounds).
The prototype was powered by a Tumansky R-15B-300 axial-flow turbojet engine with a five-stage compressor and single-stage turbine. It produced 22,500 pounds of thrust (100.1 kN) with afterburner. This was the first Soviet jet engine to use electronic engine control.
The E-152\1 had a maximum speed Mach 2.82 (2,995 kilometers per hour, 1,861 miles per hour) at 15,400 meters (50,525 feet).
The interceptor prototype had an internal fuel capacity of 4,960 liters (1,310 gallons), and the E-152\1 could carry a 1,500 liter (396 gallon) external fuel tank, giving a maximum range of 1,470 kilometers (913 miles). The service ceiling was 22,680 meters (74,409 feet).
After a two-year test program, E-152\1 and its sistership, E-152\2 were converted to E-152M\1 and E-152M\2.
Pyotr Maksimovich Ostapenko was born at Cool (or Cold), Kabardino-Balkaria, U.S.S.R, 17 September 1928. His interest in aviation began when, at age 14, he watched an aerial battle between Soviet and German fighters. Ostapenko attended the Armavir Military Aviation School of Pilots at Amravir, Krasnodar Krai, Russia, from 1948 to 1951, and then became an instructor. In 1958 he attended the Ministry of Indutrial Aviation Test Pilot School at Zhukovsky. He was a test pilot for the Mikoyan Design Bureau from 1958 to 1983.
On 26 April 1971, Ostapenko was named Hero of the Soviet Union for his heroism in testing new aviation technology. He was also awarded the Order of Lenin and the FAI’s Henry De La Vaulx Medal.
Pyotr Maksimovich Ostapenko flew more than 5,000 hours as a test pilot in more than 60 aircraft types. He held seven FAI speed, altitude and time to altitude world records. He died 8 April 2012 at the age of 83 years.