Stammlager Luft III prison in Province of East Silesia, World War II. (Muzeum Obózow Jenieckich W Żaganiu)
24 March 1944: At about 2230 hours, the first of 76 Allied prisoners of war interred at Stammlager LuftIII (Stalag Luft III) began to escape through a 30-foot-deep (9 meters), 320-foot-long (98 meters) tunnel, code-named “Harry.”
Aerial reconnaissance image of Stalag Luft III, 17 September 1944. (American Air Museum in Britain UPL 36335)
The prison, located just south of Sagan (Żagań) in East Silesia (now a part of Poland) was specially constructed to house captured Royal Air Force and other Allied airmen, and was controlled by the German air force, the Luftwaffe. Prior to this escape, the German captors had discovered at least 98 tunnels at the prison.
Popularly known as “The Great Escape,” this was the subject of a 1950 book, The Great Escape, by Paul Brickhill, who was a POW at the prison. His book was adapted into a very popular motion picture, “The Great Escape,” in 1963.
Squadron Leader Thomas Gresham Kirby-Green, RAF, and Flight Lieutenant Gordon Arthur Kidder, RCAF, were murdered by Gestapo agents near Zlín, Moravia, 29 March 1944. (This photograph may be of a reconstruction by the RAF Special Investigations Branch, circa 1946)
Jackie Cochran with her Beechcraft D17W Staggerwing, NR18562. (FAI)
24 March 1939: During a 2 hour, 26 minute flight over southern California, Jacqueline Cochran established a U.S. National Altitude Record for Women of 9,160 meters (30,052 feet). She flew a Beechcraft D17W “Staggerwing,” serial number 164, registered NR18562.¹
A National Aeronautic Association official, Larry Therkelson, took the recording barograph from the airplane and sent it to the N.A.A. headquarters in Washington, D.C., for certification. The record had previously been held by Ruth Rowland Nichols.²
“Were I to make the simple statement that I climbed to an altitude of thirty-three thousand feet, that statement in and of itself would mean nothing because I have often gone higher than that. But when I add that I did this in 1937 in a fabric-covered biplane without heating, without pressurization and without an oxygen mask, the elements of an accomplishment are added. I nearly froze; the pipestem between my teeth through which I tried to get an oxygen supply from a tank and connecting tube was inadequate for the purpose, and I became so disoriented through lack of oxygen that it took over an hour to get my bearings and make a landing. The difference between the pressure my body was accustomed to on the ground and the atmospheric pressure at 33,000 feet was such that a blood vessel in my sinus ruptured. All this was a part of the cumulative evidence that led up to cabin pressurization and and mandatory use of the oxygen mask above certain altitudes.”
— The Stars at Noon, by Jacqueline Cochran, Little, Brown and Company, Boston, 1954, Chapter IV at Pages 61–62.
According to the U.S. Centennial of Flight Commission, Jackie Cochran “. . . set more speed and altitude records than any other pilot.”
Beechcraft D17W Staggerwing NR18562, c/n 164, which Jackie Cochran used to set an altitude record, 24 March 1939, at the Beechcraft factory, Wichita, Kansas, 1937. (Beech Aircraft Corporation)
The Beechcraft Staggerwing got its name because its lower wing was placed ahead of the upper wing (negative stagger). It was a fast airplane for its time and set several speed and altitude records. The Beechcraft D17W was a special version of the D17 production model. Only two were built. Jackie Cochran purchased NR18562 from Beechcraft for $20,145.
The “Staggerwing” was a single-engine, four-place biplane with an enclosed cabin and retractable landing gear, flown by a single pilot. The basic structure was a welded tubular steel framework, with wood formers and stringers. The wings and tail surfaces were built of wood spars and ribs. The airplane was covered with doped fabric, except the cabin and engine, which were covered in sheet metal.
Beech Aircraft Corporation Model 17 “Staggerwings” under construction. (Beech B-111/U.S. Air Force)
The D17W was 26 feet, 15/32 inch (8.0677 meters) long with a wingspan of 32 feet, 0 inches (9.754 meters) and overall height of 8 feet, 0 inches (2.438 meters). It had an empty weight of 2,553 pounds (1,158 kilograms) and loaded weight of 4,200 pounds (1,905 kilograms).
While most biplanes had staggered wings, the Staggerwing was unusual in having negative stagger. (The upper wing was “staggered” aft of the lower wing.) This not only increased the pilot’s field of vision, but improved the airplane’s stability in a stall. The leading edge of the Model 17 upper wing was 2 feet, 1–19/32 inches (0.65008 meters) aft of the lower wing. The leading edges had 0° 0′ sweep. Both wings had an angle of incidence of 5° 5′. The upper wing had no dihedral, but the lower wing had +1°. The mean vertical gap between the wings was 5 feet (1.52 meters), and the chord of both wings was 5 feet, 0 inches (1.524 meters). The total wing area was 269.5 square feet (25.04 square meters). The horizontal stabilizer had 0° incidence, while the vertical fin was offset 0° 43′ to the left of the airplane’s centerline.
The Staggerwing was offered with a selection of engines of different displacements and horsepower ratings. The standard Beechcraft D17S was equipped with an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liters) Pratt & Whitney Wasp Jr. A, a direct-drive nine-cylinder radial engine producing 300 horsepower at 2,000 r.p.m at Sea Level.
The D17W was equipped with an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liters) Pratt & Whitney Wasp Junior SC-G, an experimental version of the Wasp C with a compression ratio of 6.7:1. It had 3:2 propeller reduction gearing, and drove a two-blade constant-speed Hamilton Standard propeller. The SC-G produced 525 horsepower at 2,700 r.p.m. at 9,500 feet (2,896 meters), and 575 horsepower at 2,850 r.p.m. These ratings were achieved using 87-octane gasoline. Using 100-octane aviation gasoline, the SC-G was rated at 600 horsepower at 2,850 r.p.m. for takeoff. The engine was 3 feet, 9.469 inches (1.1549 meters) long, 3 feet, 10.75 inches (1.1875 meters) in diameter, and weighed 864 pounds (391.9 kilograms).
The D17W had a maximum speed of 235 miles per hour (378 kilometers per hour) at 13,500 feet (4,115 meters). Its fuel capacity was 120 gallons (454 liters). It could climb at a maximum rate of 2,500 feet per minute (12.7 meters per second) and had a service ceiling of 30,000 feet (9,144 meters).
Jackie Cochran with her Beechcraft D17W Staggerwing, NR18562, circa 1937. A celebratory garland of flowers has been draped over the airplane’s cowl. Miss Cochran is holding what appears to be a check. (San Diego Air & Space Museum, Cliff Henderson Collection, CF_09-0050)
Jackie Cochran flew this same D17W, NR18562, in the 1937 Bendix Trophy Race, held 3 September 1937. She finished in third place with an elapsed time of 10 hours, 29 minutes, 8 seconds, averaging 194.740 miles per hour (313.404 kilometers per hour). She won a $5,500 prize.
Max Arthur Constant flew Miss Cochran’s Staggerwing in the 1938 Bendix Trophy Race. He finished in fourth place with an elapsed time of 10 hours, 14 minutes, 39 seconds, averaging 199.330 miles per hour (320.791 kilometers per hour).
Beechcraft D17W c/n 164, was impressed into military service at Tarrant Field, Texas, 12 March 1943. Assigned to the United States Army Air Corps, it was given the designation UC-43K Traveler and Air Corps serial number 42-107277. It was turned over to the Reconstruction Finance Corporation, 22 November 1944, for sale to the civil market. The airplane was now powered by a 971.930-cubic-inch displacement (15.927 liter) Wright R-975-5 Whirlwind nine-cylinder radial and was redesignated Beechcraft D17R. The Staggerwing was sold to the Carver Pump Company, Muscatine, Iowa, and registered NC50958.
The record-setting Beechcraft Staggerwing crashed at Avenger Field, Sweetwater, Texas, 15 December 1945.
Jackie Cochran’s Beechcraft D17W, NX18562, c/n 164, carrying the race number “33” circa 1938. (Unattributed)
¹ This is not the same D17W that Jackie Cochran used to set A U.S. National Speed records, 26 and 29 July 1937. Please see TDiA at: https://www.thisdayinaviation.com/26-july-1937/
² FAI Record File Number 12228: 8,761 meters (28,743 feet), 6 March 1931. Please see TDiA at: https://www.thisdayinaviation.com/6-march-1931/
Gemini III lifts off at Launch Complex 19, Cape Kennedy Air Force Station, Cape Canaveral, Florida, 14:24:00 UTC, 23 March 1965. (NASA)
23 March 1965: At 14:24:00.064 UTC, Gemini III was launched aboard a Titan II GLV rocket from Launch Complex 19 at the Cape Kennedy Air Force Station, Cape Canaveral, Florida. Major Virgil Ivan (“Gus”) Grissom, United States Air Force, a Project Mercury veteran, was the Spacecraft Commander, and Lieutenant Commander John Watts Young, United States Navy, was the pilot.
The purpose of the mission was to test spacecraft orbital maneuvering capabilities that would be necessary in later flights of the Gemini and Apollo programs
The spacecraft entered a 100.2 mile (161.2 kilometer) × 139.3 mile (224.2 kilometer) orbit, with an orbital period of 88 minutes, 18 seconds. At the end of the first orbit, Grissom used the Orbital Attitude and Maneuver System (OAMS) to move Gemini III into a 98.2 mile (158 kilometer) × 105 mile (169 kilometer) near circular orbit. During the third orbit, the spacecraft descended to 52 miles (84 kilometers) to allow normal orbital decay should the retro rocket system fail.
Gemini III made three orbits of the Earth, and splashed down after 4 hours, 52 minutes, 31 seconds. Miscalculations of the Gemini capsule’s aerodynamics caused the spacecraft to miss the intended splash down point by 69 miles (111 kilometers). Gemini III splashed down in the Atlantic Ocean at N. 22.43°, W. 70.85°, northeast of the Turks and Caicos Islands. The recovery ship was the Essex-class aircraft carrier USS Intrepid (CVS-11).
Gus Grissom would later command the flight crew of Apollo 1. He was killed with his crew during the tragic fire during a pre-launch test, 27 January 1967.
John Young served as Spacecraft Commander for Gemini 10, Command Module Pilot on Apollo 10, back-up commander for Apollo 13, commander Apollo 16, and back-up commander for Apollo 17. Later, he was commander of the maiden flight of the space shuttle Columbia STS-1 and again for STS-9 and was in line to command STS-61J when it was cancelled following the loss of the Space Shuttle Challenger.
The flight crew of Gemini III, Lieutenant Commander John W. Young, U.S. Navy, and Major Virgil I. Grissom, U.S. Air Force. (NASA)
The two-man Gemini spacecraft was built by the McDonnell Aircraft Corporation of St. Louis, the same company that built the earlier Mercury space capsule. The spacecraft consisted of a reentry module and an adapter section. It had an overall length of 19 feet (5.791 meters) and a diameter of 10 feet (3.048 meters) at the base of the adapter section. The reentry module was 11 feet (3.353 meters) long with a diameter of 7.5 feet (2.347 meters). The weight of the Gemini varied from ship to ship but was approximately 7,000 pounds (3,175 kilograms).
Artist’s concept of Gemini spacecraft, 3 January 1962. (NASA-S-65-893)
The Titan II GLV was a “man-rated” variant of the Martin SM-68B intercontinental ballistic missile. It was assembled at Martin’s Middle River, Maryland plant so as not to interfere with the production of the ICBM at Denver, Colorado. Twelve GLVs were ordered by the Air Force for the Gemini Program.
Titan II GLV, (NASA Mission Report, Figure 3-1, at Page 3–23)
The Titan II GLV was a two-stage, liquid-fueled rocket. The first stage was 70 feet, 2.31 inches (21.395 meters) long with a diameter of 10 feet (3.048 meters). It was powered by an Aerojet Engineering Corporation LR87-7 engine which combined two combustion chambers and exhaust nozzles with a single turbopump unit. The engine was fueled by Aerozine 50, a hypergolic 51/47/2 blend of hydrazine, unsymetrical-dimethyl hydrazine, and water. Ignition occurred spontaneously as the components were combined in the combustion chambers. The LR87-7 produced approximately 430,000 pounds of thrust (1,912.74 kilonewtons). It was not throttled and could not be shut down and restarted. Post flight analysis indicated that the first stage engine of GLV-8 had produced an average of 461,080 pounds of thrust (2,050.986 kilonewtons).
The second stage was 25 feet, 6.375 inches (7.782 meters) long, with the same diameter, and used an Aerojet LR91 engine which produced approximately 100,000 pounds of thrust (444.82 kilonewtons), also burning Aerozine 50. GLV-7’s LR91 produced an average of 102,735 pounds of thrust (456.988 kilonewtons).
The Gemini III/Titan II GLV combination had a total height of 107 feet, 7.33 inches (32.795 meters) and weighed 340,000 pounds (156,652 kilograms) at ignition.
The Gemini III spacecraft is displayed at the Grissom Memorial Museum, Spring Mill State Park, Mitchell, Indiana.
John Cunningham with the record-setting de Havilland DH.100 Vampire F.1, TG/278. Note the metal canopy with porthole. (BNPS).
23 March 1948: During a 45-minute flight over Hatfield, Hertfordshire, England, the de Havilland Aircraft Company chief test pilot, Group Captain John Cunningham, D.S.O., flew a modified DH.100 Vampire F.1 fighter to a Fédération Aéronautique Internationale (FAI) World Record for Altitude of 18,119 meters (59,446 feet).¹ Cunningham broke the record set nearly ten years earlier by Colonel Mario Pezzi in a Caproni Ca.161 biplane.² (See This Day in Aviation, 22 October 1938)
DH.100 Vampire F.1 TG/278 prior to high-altitude modifications. (de Havilland)
The de Havilland DH.100 Vampire F.1 flown by Cunningham was the fifth production aircraft, TG/278. It was built by the English Electric Company at Preston, Lancashire, with final assembly at Samlesbury Aerodrome, and made its first flight in August 1945. It was intended as a prototype photo reconnaissance airplane. The cockpit was heated and pressurized for high altitude, and a metal canopy installed.
The photo reconnaissance project was dropped and TG/278 became a test bed for the de Havilland Engine Company Ghost 2 turbojet (Halford H.2), which produced 4,400 pounds of thrust (19.57 kilonewtons) at 10,000 r.p.m. The Vampire could take the Ghost engine to altitudes beyond the reach of the Avro Lancaster/Ghost test bed already in use. The airplane’s wing tips were each extended 4 feet (1.219 meters) to increase lift.
De Havilland DH.100 Vampire F.1 TG/278 after modifications. (de Havilland)
The aircraft was stripped of paint to reduce weight. Smaller batteries were used and placed in normal ballast locations. Special instrumentation and recording cine cameras were installed in the gun compartment, and ten cylinders of compressed air for breathing replaced the Vampire’s radio equipment. At takeoff, the Vampire carried 202 gallons (765 liters) of fuel, 40 gallons less than maximum, sufficient for only one hour of flight. The takeoff weight of TG/278 was 8,400 pounds (3,810 kilograms).
John Cunningham had previously flown TG/278 to a world record 799.644 kilometers per hour (496.876 miles per hour) over a 100 kilometer course at Lympne Airport, 31 August 1947.³
TG/278 continued as a test aircraft until it was damaged by an engine fire in October 1950. It was used as an instructional airframe at RAF Halton.
De Havilland DH.100 Vampire F.1 TG/278 with high altitude modifications (de Havilland)
A standard Vampire F.1 was 9.370 meters (30 feet, 8.9 inches) long with a wingspan of 12.192 meters (40 feet, 0 inches) and overall height of 2.700 meters (8 feet, 10.3 inches). The fighter had an empty weight of 6,380 pounds (2,894 kilograms) and gross weight of 8,587 pounds (3,895 kilograms).
The basic Vampire F.1 was powered by a de Havilland-built Halford H.1B Goblin turbojet engine. This engine used a single-stage centrifugal-flow compressor and single-stage axial-flow turbine. It had a straight-through configuration rather than the reverse-flow of the Whittle turbojet from which it was derived. It produced 2,460 pounds of thrust (10.94 kilonewtons) at 9,500 r.p.m., and 3,000 pounds (13.34 kilonewtons) at 10,500 r.p.m. The Goblin weighed approximately 1,300 pounds (590 kilograms).
It had a maximum speed of 540 miles per hour (869 kilometers per hour), a service ceiling of 41,000 feet (12,497 meters) and range of 730 miles (1,175 kilometers).
The Vampire F.1 was armed with four 20 mm Hispano autocannon in the nose, with 150 rounds of ammunition per gun.
De Havilland DH.100 Vampire FB.5 three-view illustration with dimensions.Group Captain John Cunningham, Royal Air Force. (BNPS)
Group Captain John Cunningham C.B.E., D.S.O. and Two Bars, D.F.C. and Bar, A.E., D.L., F.R.Ae.S, was born 1917 and educated at Croydon. In 1935 he became an apprentice at De Havilland’s and also joined the Auxiliary Air Force, where he trained as a pilot. He was commissioned as a Pilot Officer, 7 May 1936, and was promoted to Flying Officer, 5 December 1937. Cunningham was called to active duty in August 1939, just before World War II began, and promoted to Flight Lieutenant, 12 March 1940.
While flying with No. 604 Squadron, Cunningham was awarded the Distinguished Flying Cross, 28 January 1941. He was appointed Acting Squadron Leader, Auxiliary Air Force, and was decorated with the Distinguished Service Order, 29 April 1941. The Gazette reported,
“This officer has continued to display the highest devotion to duty in night fighting operations. One night in April, 1941, he destroyed two enemy bombers during a single patrol and a week later destroyed three enemy raiders during three different patrols. Squadron Leader Cunningham has now destroyed at least ten enemy aircraft and damaged a number of others. His courage and skill are an inspiration to all.”
—The London Gazette, 29 April 1941, Page 2445 at Column 1.
His Majesty George VI, King of the United Kingdom, greets Squadron Leader John Cunningham, D.S.O., D.F.C., 1941. (BNPS)
Acting Squadron Leader Cunningham’s promotion to Squadron Leader (Temporary) became official 10 June 1941. The King approved the award of a Bar to his Distinguished Flying Cross, 19 September 1941. Squadron Leader Cunningham took command of No. 604 Squadron 1 August 1946.
On 3 March 1944 Wing Commander Cunningham received a second Bar to his Distinguished Service Order. According to The Gazette,
“Within a recent period Wing Commander Cunningham has destroyed three more hostile aircraft and his last success on the night of 2nd January, 1944, brings his total victories to 20, all with the exception of one being obtained at night. He is a magnificent leader, whose exceptional ability and wide knowledge of every aspect of night flying has contributed in large measure to the high standard of operational efficiency of his squadron which has destroyed a very large number of enemy aircraft. His iron determination and unswerving devotion to duty have set an example beyond praise.”
—The London Gazette, 3 March 1944, Page 1059 at Column 1.
Promoted to Group Captain 3 July 1944, Cunningham was the highest scoring Royal Air Force night fighter pilot of World War II, credited with shooting down 20 enemy airplanes. He was responsible for the myth that eating carrots would improve night vision.
In addition to the medals awarded by the United Kingdom, he also held the United States Silver Star, and the Union of Soviet Socialist Republics Order of the patriotic War (1st Class).
Following the War, John Cunningham returned to de Havilland as a test pilot. After the death of Geoffrey Raoul de Havilland, Jr., in 1946, Cunningham became the de Havilland’s chief test pilot. He remained with the firm through a series of mergers, finally retiring in 1980.
Cunningham was appointed an Officer of the Most Excellent Order of the British Empire (O.B.E.) in 1951, and promoted to Commander of the Most Excellent Order of the British Empire (C.B.E.) in 1963. He relinquished his Auxiliary Air Force commission 1 August 1967.
Group Captain John Cunningham C.B.E., D.S.O. and Two Bars, D.F.C. and Bar, A.E., D.L., died 21 July 2002 at the age of 84 years.
Wing Commander John Cunningham, D.S.O. and two bars, D.F.C. and Bar, A.E., Auxiliary Air Force. (Test and Research Pilots, Flight Test Engineers)
¹ FAI Record File Number 9844
² FAI Record File Number 11713: 17,083 meters (56,047 feet)
![A drawing showing the proposed route of one of the escape tunnels, by wartime artist Ley Kenyon, a prisoner-of-war in Stalag Luft III at the time of the Great Escape in March 1944 [Picture: from the original drawings of Ley Kenyon 1943] (GOV.UK)](https://static.thisdayinaviation.com/wp-content/uploads/tdia/2016/03/ODD_5948.jpg.webp)
