Category Archives: Aviation

7 September 1965

Aviation, , , , , , , , , , , , , , , ,
Bell Model 209 prototype, N209J, in flight with skids retracted. (Bell Helicopter Co.)
Bell Model 209, N209J, prototype of the AH-1G Huey Cobra attack helicopter, in flight with landing skids retracted. (Bell Helicopter Company)

7 September 1965: First flight of the prototype Bell Model 209 attack helicopter. Test pilot William Thomas (“Bill”) Quinlan was in command. The duration of the flight was twelve minutes.

The Model 209 was a private venture, built in just seven months and rolled out at Fort Worth, Texas, 2 September 1965. The prototype aircraft combined the drive system, rotors and tail boom of the production UH-1C gunship with a streamlined fuselage which placed the two pilots in tandem.

The prototype was equipped with retractable landing gear which gave the 209 increased speed, but the expense and complexity were enough that this feature was not included on production aircraft.

This helicopter would be developed into the famous AH-1G Huey Cobra.

N209J,the Bell Model 209 prototype, shown in camouflage colors. (Bell Helicopter Company)
N209J, the Bell Model 209 prototype, shown in camouflage colors. (Bell Helicopter Company)

The second prototype, AH-1G 66-15246, was used by the Army for flight testing at Edwards Air Force Base, California, from 3 April to 21 April 1967.

66-15246 had an overall length of 52 feet, 11.65 inches (16.146 meters) with rotors turning. The fuselage was 44 feet, 5.20 inches (13.433 meters) long, and it was 3 feet, 0 inches (0.914 meters) wide. The HueyCobra had a short “stub wing” with a span of 10 feet, 11.60 inches (3.343 meters). Its angle of incidence was 14°. The wing’s area was 27.8 square feet (2.6 square meters). 66-15426 had an empty weight of 5,516 pounds (2,502 kilograms) and maximum gross weight of 9,500 pounds (4,309 kilograms).

Bell Model 209, N209J, prototype of the AH-1G Cobra, with landing skids extended. (U.S. Army)

The two-bladed Model 540 “door-hinge” main rotor was 44 feet, 0 inches (13.411 meters) in diameter. The blades had a chord of 2 feet, 3 inches (0.686 meters) and 10° negative twist. The main rotor turned counter-clockwise when viewed from above. (The advancing blade is on the helicopter’s right.) Normal rotor r.p.m. (power on) was 314–324 r.p.m., and power off, 304–339 r.p.m. The minimum transient rotor speed, power off, was 250 r.p.m.

The two blade tail rotor assembly had a diameter of 8 feet, 6 inches (2.591 meters) with a chord of 8.41 inches (0.214 meters). There was no twist. It was mounted on the left side of the pylon in a pusher configuration and turned counter-clockwise as seen from the helicopter’s left. (The advancing blade is above the axis of rotation.) The tail rotor pylon was cambered to allow aerodynamic forces in forward flight to “unload” the tail rotor.

Bell AH-1G Cobra three-view drawing. (U.S. Army Aviation Systems Test Activity)

The AH-1G was powered by a Lycoming LTC1K-4 (T53-L-13) turboshaft engine rated at 1,400 shaft horsepower, though it was derated to the helicopter’s transmission limit. The T53-L-13 is a two-shaft free turbine with a 6-stage compressor (5 axial-flow stages, 1 centrifugal-flow stage) and a 4-stage axial-flow turbine (2 high-pressure stages, 2 low-pressure power turbine stages). The T53-L-13 is 3 feet, 11.9 inches (1.217 meters) long, 1 foot, 11.0 inches (0.584 meters) in diameter and weighs 549 pounds (249 kilograms).

The speed of the Cobra was effected by the armament configuration, whether “clean,” light or heavy scout, or “heavy hog.” At 5,000 feet (1,524 meters), the cruise speed in the clean configuration was 138.0 knots (158.8 miles per hour, 255.6 kilometers per hour); light scout, 134.0 knots (154.2 miles per hour, 248.2 kilometers per hour); and heavy hog, 127.0 knots (146.2 miles per hour, 235.2 kilometers per hour). The maximum airspeed in level flight was 149.0 knots (171.5 miles per hour, 276.0 kilometers per hour); 144.0 knots (165.7 miles per hour, 266.7 kilometers per hour); and 136.5 knots (157.1 miles per hour, 252.8 kilometers per hour), respectively.

The limiting airspeed (VNE) was 190 knots (KCAS) (219 miles per hour, 352 kilometers per hour) below 3,000 feet (914 meters) density altitude.

In autorotation, the airspeed for the minimum rate of descent was 74.0 knots (85.2 miles per hour, 137.1 kilometers per hour) with the main rotor turning 294 r.p.m., resulting in a rate of descent of 1,750 feet per minute (8.89 meters per second).

Bell AH-1G Cobra. (U.S. Army)

The basic armament for the AH-1G Cobra was an Emerson M28 turret which could be equipped with one or two General Electric M134 Miniguns, or a combination of a Minigun with a Philco Ford M129 automatic grenade launcher, or two grenade launchers. Each Minigun was supplied with 4,000 rounds of 7.62 NATO ammunition, while a grenade launcher had 300 rounds of 40 × 53 millimeter high-velocity explosive ammunition.

Four hardpoints on the stub wing could be loaded with M18 7.62 NATO Minigun pods; XM35 pods, containing a short-barreled General Electric XM195 20 millimeter Gatling gun (a variant of the M61 Vulcan); rocket pods with seven or nineteen 2.75-inch unguided rockets.

The prototype Cobra, Bell Model 209 N209J, is in the collection of the U.S. Army Aviation Museum, Fort Rucker, Alabama, as is the second prototype, 66-15246.

© 2017, Bryan R. Swopes

7 September 1961

Aviation, , , , , , ,
Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)
Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, 1961. (U.S. Air Force)

7 September 1961: As a consultant to Northrop Corporation, Jackie Cochran flew a T-38A-30-NO Talon, 60-0551, to a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a Closed Circuit of 500 Kilometers, flying from Edwards Air Force Base, California to Beatty, Nevada, Lone Pine, California, and back to Edwards. Her speed averaged 1,095.56 kilometers per hour (680.749 miles per hour).

Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)
Jacqueline Cochran’s Diplôme de Record in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)

Air Force test pilot Chuck Yeager kept notes during these record runs:

September 7: Re-run 500 km. Good run. Observers miss her at Lone Pine, Calif.

— Brigadier General Charles Elwood (“Chuck”) Yeager, U.S. Air Force, quoted in Jackie Cochran: An Autobiography, by Jacqueline Cochran and Maryann Bucknum Brinley, Bantam Books, New York, 1987, Page 305.

During August and September 1961, Cochran set series of speed, altitude and distance records with the T-38.

The Northrop T-38A Talon is a two-place, twin-engine jet trainer capable of supersonic speed. It is 46 feet, 4 inches (14.122 meters) long with a wingspan of 25 feet, 3 inches (7.696 meters) and overall height of 12 feet, 10 inches (3.912 meters). The trainer’s empty weight is 7,200 pounds (3,266 kilograms) and the maximum takeoff weight is 12,093 pounds (5,485 kilograms).

The T-38A is powered by two General Electric J85-GE-5 turbojet engines. The J85 is a single-shaft axial-flow turbojet engine with an 8-stage compressor section and 2-stage turbine. The J85-GE-5 is rated at 2,680 pounds of thrust (11.921 kilonewtons), and 3,850 pounds (17.126 kilonewtons) with afterburner. It is 108.1 inches (2.746 meters) long, 22.0 inches (0.559 meters) in diameter and weighs 584 pounds (265 kilograms).

It has a maximum speed of Mach 1.08 (822 miles per hour, 1,323 kilometers per hour) at Sea Level. The Talon’s service ceiling of 55,000 feet (16,764 meters) and it has a maximum range of 1,093 miles (1,759 kilometers).

In production from 1961 to 1972, Northrop has produced nearly 1,200 T-38s. As of January 2014, the U.S. Air Force had 546 T-38A Talons in the active inventory. It also remains in service with the U.S. Navy, and the National Aeronautics and Space Administration.

Jackie Cochran’s record-setting T-38 is in the collection of the Smithsonian Institution, National Air and Space Museum.

Northrop T-38A-30-NO Talon at Edwards Air Force Base, California. (U.S. Air Force)
Northrop T-38A-30-NO Talon 60-0551 at Edwards Air Force Base, California. (U.S. Air Force)

© 2017, Bryan R. Swopes

7 September 1956

Aviation, , , , , , , , , , , , , ,
Captain Iven Carl Kincheloe, Jr., United States Air Force
Captain Iven Carl Kincheloe, Jr., United States Air Force

7 September 1956: At Edwards Air Force Base, California, test pilot Captain Iven Carl Kincheloe, Jr., U.S. Air Force, flew the Bell X-2 rocketplane, serial number 46-674, to a speed of Mach 1.7 and an altitude of 126,200 feet (38,465 meters). He was the first pilot to fly above 100,000 feet (30,480 meters) and was called “The First of the Spacemen.”

The X-2 was a joint project of the U.S. Air Force and NACA (the National Advisory Committee for Aeronautics, the predecessor of NASA). The rocketplane was designed and built by Bell Aircraft Corporation of Buffalo, New York, to explore supersonic flight at speeds beyond the capabilities of the earlier Bell X-1 and Douglas D-558-2 Skyrocket. In addition to the aerodynamic effects of speeds in the Mach 2.0–Mach 3.0 range, engineers knew that the high temperatures created by aerodynamic friction would be a problem, so the aircraft was built from Stainless Steel and K-Monel, a copper-nickel alloy.

Bell X-2 46-674 on approach to land. (NASA ED06-0174)

The Bell Aircraft Corporation X-2 was 37 feet, 10 inches (11.532 meters) long with a wingspan of 32 feet, 3 inches (9.830 meters) and height of 11 feet, 10 inches (3.607 meters). Its empty weight was 12,375 pounds (5,613 kilograms) and loaded weight was 24,910 pounds (11,299 kilograms).

The X-2 was powered by a throttleable Curtiss-Wright XLR25-CW-1 rocket engine that produced 2,500–15,000 pounds of thrust (11.12–66.72 kilonewtons) burning alcohol and liquid oxygen. The engine used two rocket chambers and had pneumatic, electrical and mechanical controls. The smaller chamber could produce a maximum 5,000 pounds of thrust, and the larger, 10,000 pounds (22.24 and 44.48 kilonewtons, respectively).

Professor Robert H. Goddard, “The Father of Modern Rocketry,” authorized Curtiss-Wright to use his patents, and his rocketry team went to work for the Curtiss-Wright Rocket Department. Royalties for use of the patents were paid to the Guggenheim Foundation and Clark University. Professor Goddard died before he could also make the move to Curtiss-Wright.

Rather than use its limited fuel capacity to take off and climb to altitude, the X-2 was dropped from a modified heavy bomber as had been the earlier rocketplanes. A four-engine Boeing B-50A Superfortress bomber, serial number 46-011, was modified as the ”mothership.” A second Superfortress, B-50D-95-BO 48-096, was also modified to carry the X-2, and was redesignated EB-50D

The launch altitude was 30,000 feet (9,144 meters). After the fuel was exhausted, the X-2 glided to a touchdown on Rogers Dry Lake at Edwards Air Force Base.

The Bell X-2 carried by Boeing EB-50D Superfortress 48-096. (U.S. Air Force)
A Bell X-2 carried by Boeing EB-50D Superfortress 48-096. (U.S. Air Force)

Iven Kincheloe was awarded the Mackay Trophy for this flight. His altitude record remained unbeaten until the X-15 Project.

Iven Kincheloe stands in front of the Bell X-2 and the entire support team at Edwards Air Force Base. The "mothership" is a highly-modified Boeing EB-50D Superfortress. Chase aircraft are a North American F-86 Sabre, Lockheed T-33 Shooting Star, North American F-100 Super Sabre. The rescue helicopter is a Sikorsky H-19.
Iven Kincheloe stands in front of the Bell X-2 and the entire support team at Edwards Air Force Base. The “mothership” is a highly-modified Boeing EB-50D Superfortress. Chase aircraft are a North American F-86 Sabre, Lockheed T-33 Shooting Star, North American F-100 Super Sabre. The rescue helicopter is a Sikorsky H-19. (NASA)

© 2017, Bryan R. Swopes

7 September 1940

Aviation, , , , , , , , , ,
A twin-engine Heinkel He 111 medium bomber over “the U-bend in the Thames, the heart of London’s dockland, and a landmark known to every Luftwaffe bomber crew” at 1748 hours GMT, 7 September 1940. (Luftwaffe photograph)

7 September 1940: at about 4:00 p.m., the Blitz of London began with the German Luftwaffe attacking the city with 348 bombers escorted by 617 fighters. After dark, a second wave of 247 bombers attacked using the fires from the earlier attack to guide them.

Hauptman Hajo Hermann reported:

“A very clear night. . . everywhere, the German bombers were swarming in. . . Everything was lit up by fires, like a huge torch in the night.” Until 7 September, orders were very strict to not bomb indiscriminately, “But now, for the first time, we were allowed to bomb regardless.”

— Duel of Eagles, Group Captain Peter Wooldridge Townsend, C.V.O., D.S.O., D.F.C. and Bar, R.A.F. Cassell Publishers Limited, London, Chapter 27 at Pages 393–394.

Approximately 1,000 Londoners were killed that first night. During the Blitz, London was bombed for 76 consecutive nights.

Smoke rises over the City of London, during the first air raid, 7 September 1940. (NARA)

German military leaders believed that England could only be defeated by invasion. Before Germany could stage a cross-channel invasion, though, it had to gain air superiority. After weeks of relentless devastating attacks against British airfields, Reichsmarschall Hermann Wilhelm Göring made a fatal mistake. He shifted to attacking population centers.

A bomb crater at the  Elephant and Castle, London, 8 September 1940. (Unattributed)

The primary purpose of the Blitz of London was to force the Royal Air Force to defend the City. Luftwaffe commanders believed that they could destroy the RAF in battle. And the RAF had to be destroyed for an invasion of England to go forward.

By the end, losses in airplanes and crews to both sides were about even, but the RAF survived, thus Germany failed in its goal. There was no invasion.

The crew of this Heinkel He 111 on its way to London is easily visible. (Luftwaffe photograph)

The Heinkel He 111 was the primary Luftwaffe bomber. It had a crew of 5 or 6. The airplane was powered by two liquid-cooled Junkers Jumo 211 inverted V-12 engines, producing 1,200 horsepower each, giving the He 111 a maximum speed of 254 miles per hour (409 kilometers per hour). The bomber was 59 feet (17.98 meters) long with a wingspan of 77 feet (23.4 meters). It was armed with three or more 7.92 mm machine guns, and could carry up to 4,400 pounds (2,000 kilograms) of bombs. It had a maximum range of 1,420 miles (2,285 kilometers).

Fires burning at the Surrey commercial Docks, 7 September 1940. (Unattributed)

The Bomb Sight Project, sponsored by the University of Portsmouth, The National Archives, and the Joint Information Systems Committee (“Jisc”), has scanned the geographic data of every bomb that fell on London from 10 July 1940 to 6 June 1941. Interactive maps can be seen at

http://bombsight.org/#15/51.5050/-0.0900

By clicking on individual icons, information on the location and type of bomb is provided.

Below is the location of every bomb which fell on London before midnight of the first night of The Blitz, 7 September 1940:

First Night of the Blitz—7th September 1940. (The Bomb Sight Project)

© 2018, Bryan R. Swopes

7 September 1931

Aviation, , , , , , , ,
Granville Brothers Gee Bee Z, NR77V, City of Springfield. (U.S. Air Force)
Lowell Richard Bayles

7 September 1931: Lowell Richard Bayles won the 1931 Thompson Trophy Race, flying the Granville Brothers Aircraft Company Gee Bee Model Z Supersportster, NR77V, named City of Springfield. The racer was painted black and yellow, and carried the race number “4” on its wings and fuselage. The air racer had qualified for the race with a two-way average speed of 267.342 miles per hour (430.245 kilometers per hour). Bayle’s average speed for the ten-lap pylon race was 236.239 miles per hour (380.190 kilometers per hour).

In addition to the Thompson Trophy, Lowell Bayles won $7,500 in prize money (equivalent to $120,653.29 in 2017). The second place pilot, James (“Jimmie”) Wedell, won $4,500, and third place went to Dale Jackson, for $2,000.

The Gee Bee Model Z was designed by aeronautical engineer Robert Leicester Hall. Bob Hall would later become the Chief Engineer and Chief Test Pilot for the Grumman Aircraft Engineering Corporation. He was responsible for the design of Grumman’s F4F Wildcat, F6F Hellcat, F7F Tigercat, F8F Bearcat and F9F Panther and Cougar fighters, and the TBF Avenger torpedo bomber.

Bob Hall also competed in the 1931 Thompson race, flying a Gee Bee Y, number 54. He finished in fourth place, with a speed of 201.250 miles per hour (323.880 kilometers per hour).

Aeronautical engineer Robert L. Hall flew this Gee Bee Model Y in the 1931 Thompson Trophy Race. The Gee Bee Z used a NACA cowling, however, the Y is shown with a Townend ring.  (Unattributed)

Jimmy Doolittle had won the Bendix Trophy Race with the Laird Super Solution number 400, and been favored to win the Thompson Trophy Race as well. A failed piston forced him out during the seventh lap, however.

James H. Doolittle with the Bendix Trophy-winning Laird Super Solution. (San Diego Air and Space Museum Archives)

The Granville Brothers Aircraft Company Gee Bee Model Z Supersportster, serial number Z-1, was a one-of-a-kind racing airplane. It had first flown 22 August 1931 with its designer, Bob Hall, in the cockpit. The Gee Bee Z was a single-place, single-engine, low-wing monoplane with fixed landing gear and wire-braced wings. The Model Z was 15 feet, 1 inch (4.597 meters) long,with a wingspan of 23 feet, 6 inches (7.163 meters). Its empty weight was 1,400 pounds (635 kilograms) and maximum gross weight, 2,280 pounds (1,034 kilograms). The wings had a 3° angle of incidence and 4.5° dihedral. The total wing area was 75 square feet (7.968 square meters).

The Gee Bee Z was powered by an air-cooled, supercharged, 986.749-cubic-inch-displacement (16.170 liter) Pratt & Whitney Wasp Junior nine-cylinder direct-drive radial engine (the same engine which powered the winning Laird Super Solution in the 1930 Thompson Trophy Race). The engine was enclosed by a N.A.C.A. cowling, which both reduced aerodynamic drag and improved engine cooling. The Wasp Junior was modified by Pratt & Whitney to produce 535 horsepower at 2,400 r.p.m. It turned a fixed-pitch Curtiss propeller.

The Gee Bee Z had a cruise speed of 230 miles per hour (370 kilometers per hour), and maximum speed of 270 miles per hour (435 kilometers per hour).

Granville Brothers Gee Bee Model Z, NR77V, City of Springfield. The Pratt & Whitney Wasp Junior radial engine drives a Curtiss propeller. (Unattributed)

© 2018, Bryan R. Swopes