8 November 1935

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Sir Charles Edward Kingsford Smith, MC, AFC (National Archives of Australia, A1200, L93634)
Sir Charles Edward Kingsford Smith, M.C., A.F.C. (National Archives of Australia, A1200, L93634)

On 8 November 1935: Sir Charles Edward Kingsford Smith, M.C., A.F.C., and co-pilot John Thompson Pethybridge disappeared while flying Lady Southern Cross, a Lockheed Altair 8D Special, across the Andaman Sea from Allahabad, Indian Empire, to Singapore, Straits Settlements, a distance of approximately 1,932 nautical miles (2,224 statute miles, or 3,578 kilometers). The aviators were attempting to break a speed record for flight from England to Australia.

The airplane was sighted over Calcutta, British India, at 9:06 a.m., local time.

The pilot of another airplane, Charles James (“Jimmy”) Melrose, who was also en route to Australia, reported that,

“. . . he saw a ‘plane, which must have been Kingsford Smith’s, pass about 200 feet above him at 3 o’clock this morning, when he was over the Bay of Bengal, about 150 miles from land. . . Mr. Melrose said that when he passed over him in the Bay of Bengal Kingsford Smith’s speed was double his own, which was 110 miles an hour. It gave him an uncanny feeling over the desolate ocean to see the spurts of flame coming from the twin exhausts of the Lady Southern Cross. . . Kingsford Smith’s altitude was between 8000 and 9000 feet.”

—The Sydney Morning Herald, No. 30,531, Saturday, 9 November 1935, Page 19, Columns 7 and 8

On 1 May 1937, about eighteen months after the disappearance, two Burmese fisherman found a landing gear assembly floating in the Andaman Sea near Kokunye Kyun (Aye Island), off the west coast of Burma. Lockheed was able to confirm that it was from Lady Southern Cross. The component is in the collection of the Powerhouse Museum, Sydney, Australia.

Landing gear assembly of Kingsford Smith’s Lady Southern Cross is in the collection of the Powerhouse Museum venue of the Museum of Applied Arts and Sciences. (MAAS Collection 94/64/1)

In 2009, searchers claimed to have located the wreck of the airplane near the island, but this has not been confirmed.

Lockheed 8-D Altair VH-USB, Lady Southern Cross, at Burbank, California, September 1935. (Unattributed)
Lockheed Altair 8D Special VH-USB, Lady Southern Cross, at Burbank, California, September 1935. The Altair is “. . . painted consolidated blue with silver wing and silver striping. . . .” (David Horn Collection No. 9099)

Kingsford Smith was a former Royal Air Force pilot and flight instructor. He had been a barnstormer, airline pilot, and gained world-wide fame for his trans-Pacific flights. From 31 May to 9 June 1928 he and Charles Ulm, Harry Lyon and James Warner had flown Southern Cross, a Fokker F.VIIB/3m, from Oakland, California to Brisbane, with stops at Hawaii and Fiji. In 1934, with Lady Southern Cross, he and Patrick Gordon Taylor flew from Australia to Hawaii and on to Oakland, California, arriving 4 November.

Charles Kingsford Smith’s Lady Southern Cross at Lockheed, Burbank, California. Note the navigator’s sighting lines on the elevators. (Code One Magazine/Lockheed Martin)

After the transpacific flight, Lady Southern Cross spent the next 11 months at Lockheed being repaired and overhauled. Kingsford Smith then flew it across the United States and had it transported to England aboard a ship.

Lady Southern Cross was a Lockheed Altair 8D Special, a single-engine monoplane with the fuselage, wings and tail surfaces built of spruce. The Altair had been modified from a 1930 Lockheed Sirius 8A Special, NR118W, c/n 152, which was an airplane with fixed landing gear. Lockheed designed a new wing which included retractable landing gear, operated by a hand crank from the cockpit. The Sirius and Altair were single-place utility transports. Kingsford Smith’s Altair was further modified with two cockpits in tandem. Lady Southern Cross was painted Consolidated Blue (a dark blue color) with silver accents.

Sir Charles Edward Kingsford Smith, MC, AFC, with the Lady Southern Cross at Croydon, 17 October 1935. The airplane's registration has been changed to G-ADUS.
Air Commodore Sir Charles Edward Kingsford Smith, Kt, MC, AFC, with the Lady Southern Cross at Croydon, 17 October 1935. The airplane’s registration has been changed to G-ADUS. (PHOTOSHOT)

Lady Southern Cross had a length of 27 feet, 10 inches (8.484 meters) with a wingspan of 42 feet, 9¼ inches (13.037 meters) and height of 9 feet, 3 inches (2.819 meters). The modified airplane had an empty weight of 3,675 pounds (1,667 kilograms) and a maximum gross weight of 6,700 pounds (3,039 kilograms).

The airplane’s standard Pratt & Whitney Wasp C1 engine was replaced at Kingsford Smith’s request with a more-powerful Pratt & Whitney Wasp SE, serial number 5222. The Wasp SE was an air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) single-row 9-cylinder radial engine with a compression ratio of 6:1. It was rated at 500 horsepower at 2,200 r.p.m., at an altitude of 11,000 feet (3,353 meters). The SE was a direct-drive, right-hand tractor engine which turned a two-bladed Hamilton Standard controllable-pitch metal propeller with a diameter of 9 feet, 0 inches (2.743 meters). The Wasp SE was 3 feet, 6.59 inches (1.082 meters) long, 4 feet, 3.44 inches (1.307 meters) in diameter and weighed 750 pounds (340.2 kilograms).

An Altair 8D  had a cruising speed of 175 miles per hour (282 kilometers per hour) and a maximum speed of 207 miles per hour (333 kilometers per hour) at 7,000 feet (2,134 meters). Contemporary news reports stated that Kingsford Smith had reached speeds of 230 miles per hour (370 kilometers per hour) while testing VH-USB.

Sir Charles Edward Kingsford Smith, MC, AFC, At Lympne Airport, Kent, England, 6 November 1935. This may be the last photograph ever taken of "Smithy". (International News Photos)
Air Commodore Sir Charles Edward Kingsford Smith, Kt, MC, AFC, at Lympne Airport, Kent, England, 6 November 1935. This may be the last photograph ever taken of “Smithy.” (International News Photos)

© 2017, Bryan R. Swopes

7 November 1945

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Gloster Meteor F Mk.IV, EE455, Brittania, 1945. (Gloster Aircraft Co., Ltd.)

7 November 1945: Wing Commander Hugh Joseph Wilson, A.F.C. and Two Bars, Royal Air Force, Commandant of the Empire Test Pilots’ School at RAF Cranfield, set the first world speed record with a jet-propelled airplane, and the first speed record by an airplane in excess of 600 miles per hour (965.606 kilometers per hour), when he flew the Gloster Meteor F Mk.IV, EE454, to 975.68 kilometers per hour (606.26 miles per hour)—0.80 Mach—at an altitude of 75 meters (246) above Sea Level.

The course was an 8 mile (12.9 kilometers) straight away from the Herne Bay Pier to Reculver Point, along the south coast of the Thames Estuary. This was a new Fédération Aéronautique Internationale (FAI) record for speed over a 3 kilometer course. ¹

Gloster Meteor Mk.III EE457, sistership of the two record-setting Mk.IV prototypes. (Unattributed)
Gloster Meteor F Mk.III EE457, sister ship of the two record-setting Mk.IV prototypes. (Unattributed)

Months of preparation by both the Royal Air Force, which formed a special “flight,” and Gloster Aviation Co., Ltd., went into the speed record effort. Two Meteor F Mk.III fighters, EE454 and EE455, were modified to the new Mk.IV version to attempt the speed record.

Gloster Meteor F Mk.III EE455 prior to modification to Mk.IV. © IWM (ATP 15305D)

The standard B.37 Rolls-Royce Derwent Series I turbojet engines were replaced with Derwent Series V turbojets and lengthened jet nacelles. The wings were shortened, the tips reshaped and the canopy was cut down and strengthened. All trim tabs on flight control surfaces were disabled and their edges sealed. Landing gear and gear door up-latches were strengthened to prevent them from being sucked open at high speed. The airplanes were lightened and all armament deleted. The surfaces were smoothed and painted in a gloss finish. EE454 retained the standard camouflage pattern, while EE455 was painted in a distinctive yellow-gold color.

Many hours of flight testing were performed to ensure that the airplanes would be stable enough at high speeds while flying at the very low altitude required by the Fédération Aéronautique Internationale‘s rules. The slightest deviation from smooth flight could have disastrous results.

Group Captain Hugh J. Wilson CBE AFC with Gloster Chief Test Pilot Eric Stanley Greenwood OBE. (Photograph courtesy of Neil Corbett, Test & Research Pilots, Flight Test Engineers)
Wing Commander Hugh Joseph Wilson, A.F.C. and Two Bars, with Gloster Chief Test Pilot Eric Stanley Greenwood. (Photograph courtesy of Neil Corbett, Test & Research Pilots, Flight Test Engineers)

EE454 was flown by Wing Commander Hugh Joseph Wilson, A.F.C. and Two Bars (three awards), and EE455 by Gloster Chief Test Pilot Eric Stanley Greenwood. Each airplane was required to make four passes over the 3 kilometer (1.8641 statute miles) course, with two runs in each direction. The airplanes were required to remain at or below 75 meters (246 feet) during the runs over the course, and during the turns at the end of each run, below 400 meters  (1,312 feet).

On the day of the speed runs, the weather was marginal. It was cold and overcast, and visibility varied from 7 to 12 miles 11–19 kilometers) along the course. The wind was 8–12 miles per hour (3.6–5.4 meters per second) from the northwest.

Wilson made four passes over the course. His speeds for each run were 604, 608, 602 and 611 miles per hour (972, 978, 969, and 983 kilometers per hour). Greenwood made his speed runs an hour later. His runs were 599, 608, 598 and 607 miles per hour (964, 978, 962 and 977 kilometers per hour).

Wilson’s average speed was the higher of the two. His official FAI-homologated record speed is 975.68 kilometers per hour (606.26 miles per hour). Greenwood’s average speed was 970.63 kilometers per hour (603.122 miles per hour.).² Both pilots are credited with official FAI world speed records.

Color photograph of Gloster Meteor Mk.IV EE455 (RAF Museum)

Post-flight inspections revealed that the sheet metal of the Meteors’ engine intakes had significantly distorted by the intense pressure differentials experienced during the speed runs.

The B.37 Rolls-Royce Derwent Series V, interestingly, was not a direct development of the preceding Derwent Series I–IV engines. Instead, it was a scaled-down version of the RB.41 Nene, which was in turn, a scaled-up and improved Derwent I. The Derwent V had a single-stage, two-sided, centrifugal-flow compressor and a single-stage axial-flow turbine. The compressor impeller and turbine rotor were mounted on a single shaft which was supported on each end by roller bearings, and in the center by a ball bearing. The Derwent V used nine combustion chambers, and burned aviation kerosene. Engine lubricating oil was added to the fuel at a 1:100 ratio, by volume. The Series V had a Normal Power rating of 3,000 pounds of thrust (13.345 kilonewtons) at 14,000 r.p.m., and a Take-off or Military Power rating of 3,500 pounds of thrust (15.569 kilonewtons) at 14,600 r.p.m. (There was no time limit for this power setting.) The engine produced a maximum 4,000 pounds of thrust (17.793 kilonewtons) at 15,000 r.p.m. at Sea Level. During the speed runs, thrust was restricted to 3,600 pounds (16.014 kilonewtons) on both Meteors. The Derwent V engine was 7 feet, 4.5 inches (2.248 meters) long, 3 feet, 7 inches (1.092 meters) in diameter and weighed 1,280 pounds (581 kilograms).

(Rolls-Royce named its piston aircraft engines after predatory birds, e.g., Kestrel, Merlin, but its turbine engines were named after rivers.)

Gloster Meteor Mk. IV EE455 on jack stands. (Unattributed)
Gloster Meteor F Mk. IV EE455 on jack stands. (Unattributed)
Gloster Meteor F Mk. IV EE455 on jack stands. (Unattributed)

British Pathé news film of the speed runs can be seen at:

Group Captain Wilson was born at Westminster, London, England, 28 May 1908, the only son of Alfred Wilson and Jessie Wood Young Wilson. He was educated at the University School, Hastings, and the Merchant Taylors’ School, London.

Wilson received a short service commission as a Pilot Officer in the Royal Air Force, 13 September 1929 and was assigned to the No. 5 Flight Training School, at RAF Sealand, Flintshire, Wales. Pilot Officer Wilson was then assigned to 111 Squadron at Hornchurch, Essex, 1930–1932. He was promoted to Flying Officer, 13 March 1931. From 1932 to to 1934, “Willie” Wilson was assigned to the School of Naval Co-operation and Air Navigation at Lee-on-Solent, Hampshire.

On the completion of his five-year short service, Wilson was transferred to the Reserve Air Force Officers list. He qualified in flying boats and acted as a flight instructor for the RAF Reserve School. Wilson was promoted to Flight Lieutenant 1 April 1937, with seniority retroactive to 1 April 1936.

Flying Officer Wilson in the cockpit of a Blackburn Roc fighter.
Flying Officer Hugh Wilson in the cockpit of a prototype Blackburn Roc fighter, RAF Northolt, 22 May 1939.

While a reserve officer, Wilson was a test pilot for Blackburn Aircraft Ltd., and made the first flight of the Blackburn Roc. He then became a civil test pilot at the Royal Aircraft Establishment, Farnborough.

In 1939 Flight Lieutenant Wilson was recalled to active duty. He was assigned as Commanding Officer, Aerodynamic Flight, RAE Farnborough, and also flew with No. 74 Fighter Squadron at Biggin Hill. On 1 September 1940, Wilson was promoted to the rank of Squadron Leader. In 1941, Wilson was appointed chief test pilot at the Royal Aircraft Establishment and was responsible for testing all captured enemy aircraft. He was promoted to Wing Commander, 20 August 1945.

Squadron Leader Hugh J. Wilson, AFC and Bar, in teh cocpit of a captured Focke-Wulf Fw 190A3, Werke Number 313, in RAF markings as MP499. (Royal Air Force)
Squadron Leader Hugh J. Wilson, A.F.C. and Bar, in the cockpit of a captured Focke-Wulf Fw 190A 3, W.Nr. 313, in RAF markings as MP499, August 1942. (Detail from Imperial War Museum photograph)
CBE medal with Military ribbon.
Commander of the Order of the British Empire Medal with Military Division Ribbon. (Wikipedia)

Wing Commander Hugh Joseph Wilson, A.F.C. and Two Bars, Royal Air Force, was named Commander of the Most Excellent Order of the British Empire (C.B.E.) in the King’s Birthday Honours List, 13 June 1946.

On 22 February 1947, Wing Commander Wilson married Mrs. Moira Garnham (the former Miss Thom Isobel Moira Sergeant). They had one son. On 4 December 1959, he married Miss Patricia Frances Stanley Warren. They had two children.

Wing Commander Hugh J. Wilson retired from the Royal Air Force at his request 20 June 1948, with the rank of Group Captain. He died at Westminster, London 5 September 1990 at the age of 82 years.

Gloster Chief Test Pilot Eric Stanley “Terry” Greenwood (29 November 1908–February 1979) was the first pilot to exceed 600 miles per hour, while test flying the Meteors. He was appointed an Officer of the Most Excellent Order of the British Empire (O.B.E.) in the King’s Birthday Honours List, 13 June 1946.

¹ FAI Record File Number 9847

² FAI Record File Number 9846

© 2023 Bryan R. Swopes

6 November 1958

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Bell X-1E 46-063 on Rogers Dry Lake. (NASA)
Bell X-1E 46-063 on Rogers Dry Lake, 1955. (NASA)

6 November 1958: NASA Research Test Pilot John B. (Jack) McKay made the final flight of the X-1 rocketplane program, which had begun twelve years earlier.

Bell X-1E 46-063 made its 26th and final flight after being dropped from a Boeing B-29 Superfortress over Edwards Air Force Base on a flight to test a new rocket fuel.

John B. McKay, NACA/NASA Research Test Pilot. (NASA)
John B. McKay, NACA/NASA Research Test Pilot. (NASA)

When the aircraft was inspected after the flight, a crack was found in a structural bulkhead. A decision was made to retire the X-1E and the flight test program was ended.

The X-1E had been modified from the third XS-1, 46-063. It used a thinner wing and had an improved fuel system. The most obvious visible difference is the cockpit, which was changed to provide for an ejection seat. Hundreds of sensors were built into the aircraft’s surfaces to measure air pressure and temperature.

The Bell X-1E was 31 feet (9.449 meters) long, with a wingspan of 22 feet, 10 inches (6.960 meters). The rocketplane’s empty weight was 6,850 pounds (3,107 kilograms) and fully loaded, it weighed 14,750 pounds (6,690 kilograms). The rocketplane was powered by a Reaction Motors XLR11-RM-5 rocket engine which produced 6,000 pounds of thrust (26.689 kilonewtons). The engine burned ethyl alcohol and liquid oxygen. The X-1E carried enough propellants for 4 minutes, 45 seconds burn.

The Bell X-1E rocketplane being loaded into a Boeing B-29 Superfortress mothership for another test flight. (NASA)
The Bell X-1E rocketplane being loaded into NACA 800, a Boeing B-29-96-BW Superfortress mothership, 45-21800, for another test flight. (NASA)

The early aircraft, the XS-1 (later redesignated X-1), which U.S. Air Force test pilot Charles E. (“Chuck”) Yeager flew faster than sound on 14 October 1947, were intended to explore flight in the high subsonic and low supersonic range. There were three X-1 rocketplanes. Yeager’s Glamorous Glennis was 46-062. The X-1D (which was destroyed in an accidental explosion after a single glide flight) and the X-1E were built to investigate the effects of frictional aerodynamic heating in the higher supersonic ranges from Mach 1 to Mach 2.

Bell X-1E loaded aboard Boeing B-29 Superfortress, circa 1955. (NASA)
Bell X-1E 46-063 loaded aboard NACA 800, a Boeing B-29-96-BW Superfortress, 45-21800, circa 1955. (NASA)

The X-1E reached its fastest speed with NASA test pilot Joseph Albert Walker, at Mach 2.24 (1,450 miles per hour/2,334 kilometers per hour), 8 October 1957. Walker also flew it to its peak altitude, 70,046 feet (21,350 meters) on 14 May 1958.

NACA test pilot Joseph Albert Walker made 21 of the X-1E's 26 flights. In this photograph, Joe Walker is wearing a David Clark Co. T-1 capstan-type partial-pressure suit with a K-1 helmet for protection at high altitudes. (NASA)
NACA test pilot Joseph Albert Walker made 21 of the X-1E’s 26 flights. In this photograph, Joe Walker is wearing a David Clark Co. T-1 capstan-type partial-pressure suit with a K-1 helmet for protection at high altitudes. (NASA)

There were a total of 236 flights made by the X-1, X-1A, X-1B, X-1D and X-1E. The X-1 program was sponsored by the National Advisory Committee on Aeronautics, NACA, which became the National Aeronautics and Space Administration, NASA, on 29 June 1958.

The X-1E is on display in front of the NASA administration building at the Dryden Flight Research Center, Edwards Air Force Base, California. Bell X-1E 46-063 on display at Dryden Flight Research Center © 2016, Bryan R. Swopes

6 November 1957

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Fairey Rotodyne XE 521 photographed during its first flight, 6 November 1957. (Fairey Aviation Co., Ltd.)

6 November 1957: XE521 made its first flight at White Waltham with Squadron Leader Wilfred Ronald Gellatly, AFC, and Lieutenant Commander John George Peter Morton in the cockpit.

The Fairey Rotodyne was a unique aircraft. Like a helicopter, it was capable of hovering and low-speed translating flight. The main rotor had both cyclic and collective pitch and provided roll and pitch control. Unlike a helicopter, though, thrust for forward flight was provided by two turboprop engines. Varying the propellers’ pitch provided yaw control for the aircraft until about 80 knots, when the twin rudders were sufficiently effective. As the Rotodyne accelerated in forward flight, the stub wing provided increasing lift and at about 60 knots, the main rotor tip jets were turned off. The main rotor continued to turn in autorotation, as in a gyrocopter.

Squadron Leader Wilfred Ronald Gellatly, AFC, leans out of the cockpit after the first flight of Fairey Rotodyne XE521, 6 November 1957. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

Flight controls were similar to those of a helicopter, with a cyclic stick and collective lever with a twist throttle. The pedals, though, rather than controlling a tail rotor, varied the propeller blades’ pitch and rudder angle. The elevators were controlled by electric trim motors.

The Rotodyne’s four-blade main rotor used symmetrical airfoils. It was 90 feet (27.432 meters) in diameter and the blade tip speed was 720 feet per second (219.5 meters per second). The blades had a chord of 2 feet, 3 inches (0.686 meters). The rotor blades were built of steel for strength, fatigue life and resistance to corrosion. The leading edge spar was machined from a 35 foot rolled steel billet and the rear spar was fabricated of layered stainless steel. The airfoil is shaped by pierced stainless steel ribs. The steel skin was a single sheet, joined at the trailing edge.

The wing span was 46 feet, 6 inches (14.173 meters). The engines and main landing gear were  carried in long nacelles mounted under the wing.

The Rotodyne’s fuselage was 58 feet, 8 inches (17.812 meters) long. The cabin has a length of 46 feet (14.021 meters) and is 8 feet (2.438 meters) wide and 6 feet (1.829 meters) high, providing space for 40 passengers or up to 9,000 pounds (4,082.3 kilograms of cargo. Clamshell doors at the aft end provided for cargo loading. Overall height of the aircraft was 22 feet, 2 inches (6.756 meters).

XE521 under construction. © Hulton-Deutsch Collection/CORBIS/Corbis via Getty Images

The Rotodyne was powered by two Napier & Son Eland NEl.3 turboprop engines with a maximum rated power of 2,805 shaft horsepower and 500 pounds of thrust at 12,500 r.p.m. for takeoff. Maximum continuous power was 2,180 shaft horsepower and 420 pounds of thrust. These engines drove four-bladed Rotol propellers with a diameter of 13 feet (3.962 meters). An auxilary compressor at the rear of the engine supplied compressed air for the main rotor tip-jets. Each engine supplied power to opposite pairs of of rotor blades at 250 °C. (482 °F.)

The prototype had an empty weight of 24,030 pounds (10,899.9 kilograms)

Front view of Fairey Rotodyne with Squadron Leader Wilfred Ronald Gellatly OBE, AFC, RNZAF. (Fairey Aviation Co., Ltd.)

© 2020 Bryan R. Swopes