Tag Archives: Lockheed Aircraft Company

15 August 1935

Aviation, , , , , , , , , , , , , , ,
Will Rogers and Wiley Post with the Lockheed Model 9E Orion hybrid at Renton, Washington. The pontoons have just been installed on the airplane in place of its fixed landing gear. (Unattributed)
Will Rogers and Wiley Post with the Lockheed Model 9E Orion hybrid at Renton, Washington. The pontoons have just been installed on the airplane in place of its fixed landing gear. (Seattle Post Intelligencer Collection/Museum of History & Industry)

15 August 1935: Two of the most famous men of their time, Wiley Hardeman Post and William Penn Adair (“Will”) Rogers, were killed in an airplane crash near Point Barrow, Alaska.

Post, a pioneering aviator who had twice flown around the world—once, solo—and helped develop the pressure suit for high altitude flight, was exploring a possible air mail route from the United States to Russia. His friend, world famous humorist Will Rogers, was along for the trip.

Transcontinental and Western Airlines' Lockheed Model 9E special, NC12283. This airplane would be modified by Pacific Airmotive, Burbank, California, for Wiley Hardeman post. (Ed Coates Collection)
Transcontinental & Western Air Incorporated’s Lockheed Model 9E Special, NC12283. This airplane would be modified by Pacific Airmotive, Burbank, California, for Wiley Hardeman Post. (Ed Coates Collection)

Post’s airplane was a hybrid, built from the fuselage of a former Transcontinental & Western Air, Inc., Lockheed Model 9E Orion Special, NC12283, combined with a wing from a Lockheed Model 7 Explorer. T&WA operated the Orion for two years before selling it to Charles Babb, Glendale, California. Babb installed the salvaged wing from a modified Lockheed Model 7 Explorer, Blue Flash, NR101W, which had crashed in Panama in 1930.

The Orion’s standard 450 horsepower Pratt & Whitney Wasp SC1 engine was replaced with an air-cooled, supercharged, 1,343.8-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp S3H1 nine-cylinder radial engine (serial number 5778), rated at 550 horsepower at 2,200 r.p.m. to 5,000 feet (1,524 meters), and 600 horsepower at 2,250 r.p.m. for takeoff. A three-bladed Hamilton Standard variable-pitch propeller was used. Both the SC1 and S3H1 were direct drive engines. The S3H1 was 3 feet, 7.01 inches (1.093 meters) long and 4 feet, 3.60 inches (1.311 meters) in diameter. It weighed 865 pounds (392 kilograms).

Post also wanted to replace the retractable landing gear with pontoons for water landings.

Lockheed engineers were of the opinion that the hybrid aircraft and the other modifications which were requested by Post were dangerous and refused to do the work. Pacific Airmotive, also located in Burbank, California, however, agreed to modify the airplane. Several names were used to describe the hybrid airplane, such as “Lockheed Aurora,” as well as others perhaps less polite. It was given the restricted registration NR12283.

NR12283 was 27 feet, 6 inches (8.382 meters) long with a wingspan of 48 feet, 6 inches (14.783 meters). The wing area was 313 square feet (29.079 square meters).

Wiley Post’s red Lockheed Orion/Explorer hybrid, NR12283, at Renton, Washington.

Post had the pontoons installed at Renton, Washington. The floats that he had ordered did not arrive on time so he installed a larger set intended for another aircraft.

NR12283, Wiley Post's hybrid Lockheed Orion/Explorer float plane, at Fairbanks, Alaska. (PBS)
NR12283, Wiley Post’s red hybrid Lockheed Orion/Explorer float plane, at Fairbanks, Alaska. (PBS)

After several days of flying from Seattle and through Alaska, Post and Rogers were nearing Point Barrow on the northern coast of the continent. They encountered dense fog and landed on Walakpa Bay, about 13 miles (21 kilometers) southwest of the village of Barrow.

“August 15, 1935 2:00 p.m. — Harding Lake, Alaska. Wiley Post and Will Rogers taxi for take-off. Last photo before their 6:30 p.m. crash near Barrow. Patton Collection #13 ” (Harding Lake Association)

After talking with a local resident, Clair Okpheah, they taxied back on the lagoon and took off to the north. Post banked to the right, but at about 50 feet (15 meters) the engine stopped. NR12283 pitched down, rolled to the right, and then its right wing struck the mud. The right wing and pontoon were torn off and the airplane crashed upside down. Post and Rogers died.

Clair Okpheah ran to Barrow for help. When a rescue party arrived 16 hours after the crash, the men recovered the bodies of Post and Rogers. It was noted that Wiley Post’s wristwatch had stopped at 8:18 p.m.

Wiley Post's hybrid airplane, NR12283, after the crash, 15 August 1935. (UPI)
The wreckage of Wiley Post’s Lockheed Model 9E Orion hybrid airplane, NR12283, after the crash at Walakpa Lagoon, Alaska, 15 August 1935. (UPI)

© 2018, Bryan R. Swopes

6 August 1945

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Major Richard Ira Bong, United States Army Air Forces. (U.S. Air Force)

6 August 1945: After serving three combat tours flying the Lockheed P-38 Lightning in the Southwest Pacific, Major Richard Ira Bong, Air Corps, United States Army, was assigned as an Air Force acceptance test pilot for new Lockheed P-80 Shooting Star jet fighters at the Lockheed Air Terminal, Burbank, California.

The P-80A was a brand new jet fighter, and Major Bong had flown just 4 hours, 15 minutes in the type during 12 flights.

Shortly after takeoff in P-80A-1-LO 44-85048, the primary fuel pump for the turbojet engine failed. A back-up fuel pump was not turned on. The Shooting Star rolled upside down and Bong bailed out, but he was too low for his parachute to open and he was killed. The jet crashed at the intersection of Oxnard Street and Satsuma Avenue, North Hollywood, California, and exploded.

Site of the crash of Major Richard I. Bong’s Lockheed P-80A-1-LO fighter, 44-85048, at Oxnard Street and Satsuma Avenue, North Hollywood, California. (Contemporary news photograph)
This graphic appeared in the Los Angles Times, 7 August 1945, at Page 3. (Los Angeles Times)
General Douglas MacArthur with Major Richard I. Bong.
General Douglas MacArthur with Major Richard I. Bong.

Richard I. Bong was known as the “Ace of Aces” for scoring 40 aerial victories over Japanese airplanes between 27 December 1942 and 17 December 1944 while flying the Lockheed P-38 Lightning. He was awarded the Medal of Honor, which was presented by General Douglas MacArthur, 12 December 1944. [The following day, General MacArthur was promoted to General of the Army.]

The citation for Major Bong’s Medal of Honor reads: “For conspicuous gallantry and intrepidity in action above and beyond the call of duty in the Southwest Pacific area from 10 October to 15 November 1944. Though assigned to duty as gunnery instructor and neither required nor expected to perform combat duty, Major Bong voluntarily and at his own urgent request engaged in repeated combat missions, including unusually hazardous sorties over Balikpapan, Borneo, and in the Leyte area of the Philippines. His aggressiveness and daring resulted in his shooting down eight enemy airplanes during this period.”

General of the Army Henry H. (“Hap”) Arnold and Major Richard I. Bong, circa 1945.

The Lockheed P-80-1-LO was the United States’ first operational jet fighter. It was a single-seat, single-engine low-wing monoplane powered by a turbojet engine. The fighter was designed by a team of engineers led by Clarence L. (“Kelly”) Johnson. The prototype XP-80A, 44-83020, nicknamed Lulu-Belle, was first flown by test pilot Tony LeVier at Muroc Army Air Field (now known as Edwards Air Force Base), 8 January 1944.

Lockheed P-80A-1-LO shooting Star 44-85004, similar to the fighter being test flown by Richard I. Bong, 6 August 1945. (U.S. Air Force)

The P-80A was a day fighter, and was not equipped for night or all-weather combat operations. The P-80A was 34 feet, 6 inches (10.516 meters) long with a wingspan of 38 feet, 10.5037 inches (11.84919 meters) ¹ and overall height of 11 feet, 4 inches (3.454 meters).

The leading edges of the P-80A’s wings were swept aft 9° 18′ 33″. They had an angle of incidence of +1° at the root and -0° 30′ at the tip. There was 3° 50′ dihedral. The total wing area was 237.70 square feet (22.083 square meters).

The fighter had an empty weight of 7,920 pounds (3,592 kilograms) and a gross weight of 11,700 pounds (5,307 kilograms). The maximum takeoff weight was 14,000 pounds (6,350 kilograms).

Lockheed P-80 Shooting Star production, alongside P-38 Lightnings. (SDASM)

Early production P-80As were powered by either an Allison J33-A-9 or a General Electric J33-GE-11 turbojet engine. The J33 was a licensed version of the Rolls-Royce Derwent. It was a single-shaft turbojet with a 1-stage centrifugal compressor section and a 1-stage axial-flow turbine. The -9 and -11 engines were rated at 3,825 pounds of thrust (17.014 kilonewtons). The J33s were 8 feet, 6.9 inches (2.614 meters) long, 4 feet, 2.5 inches (1.283 meters) in diameter and weighed 1,775 pounds (805 kilograms).

The P-80A had a cruising speed of 445 miles per hour (716 kilometers per hour) at 20,000 feet (6,096 meters). Its maximum speed was 548 miles per hour (882 kilometers per hour) at 2,700 feet (823 meters) and and 501 miles per hour (806 kilometers per hour) at 34,700 feet (10,577 meters).² The service ceiling was 45,000 feet (13,716 meters).

Lockheed P-80A-1-LO Shooting Star 44-85155, similar to the jet fighter which Major Bong was flying, 6 August 1945. (U.S. Air Force)

The P-80A Shooting Star was armed with six air-cooled Browning AN-M2 .50-caliber aircraft machine guns mounted in the nose.

Dick Bong poses with “Marge,” his Lockheed P-38J Lightning. A large photograph of his fiancee, Miss Marjorie Vattendahl, is glued to the fighter’s nose.

¹ Wing span with rounded wing tips. P-80As with squared (“clipped”) tips had a wing span of 37 feet, 7.5037 inches (11.46819 meters).

² Several hundred of the early production P-80 Shooting stars had all of their surface seams filled, and the airplanes were primed and painted. Although this process added 60 pounds (27.2 kilograms) to the empty weight, the decrease in drag allowed a 10 mile per hour (16 kilometers per hour) increase in top speed. The painted surface was difficult to maintain in the field and the process was discontinued.

© 2018, Bryan R. Swopes

27 July 1976

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Lockheed SR-71A 61-7958. (FAI)
Lockheed SR-71A 61-7958. (FAI)

27 July 1976: Major Adolphus H. Bledsoe, Jr., pilot, and Major John T. Fuller, RSO, flew a Lockheed SR-71A, 61-7958, to a Fédération Aéronautique Internationale (FAI) Absolute World Record Speed of 2,092.29 miles per hour (3,367.22 kilometers per hour) over a 1,000 kilometer closed circuit.

FAI Record File Num #3928 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km without payload
Performance: 3 367.22 km/h
Date: 1976-07-27
Course/Location: Beale Air Force Base, CA (USA)
Claimant Adolphus Bledsoe (USA)
Aeroplane: Lockheed SR-71 “Blackbird” (17958)
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #3929 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 1 000 km with 1 000 kg payload
Performance: 3 367.22 km/h
Date: 1976-07-27
Course/Location: Beale Air Force Base, CA (USA)
Claimant Adolphus Bledsoe (USA)
Aeroplane: Lockheed SR-71 “Blackbird” (17958)
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

FAI Record File Num #3930 [Direct Link]
Status: ratified – superseded since approved
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-Absolute (Absolute Record of classes C, H and M)
Category: Not applicable
Group: Not applicable
Type of record: Speed
Performance: 3 367.22 km/h
Date: 1976-07-27
Course/Location: Beale Air Force Base, CA (USA)
Claimant Adolphus Bledsoe (USA)
Aeroplane: Lockheed SR-71 “Blackbird” (17958)
Engines: 2 Pratt & Whitney J-58/JTD11D-20A

De La Vaulx Medal
De La Vaulx Medal

The following day, the same airplane, flown by two different crews, set a World Record for Altitude in Horizontal Flight at 85,068 feet (25,929 meters) and a World Record for Speed Over a Straight 15/25 Kilometer Course, 2,193.17 miles per hour (3,529.56 kilometers per hour). This second speed record became the new Absolute Speed Record, superseding the record set on this date by Alphonsus Bledsoe and John T. Fuller.

All six airmen were awarded the Henry De La Vaulx Medal by the FAI.

Today, 61-7958 is on display at the Museum of Aviation, Warner-Robins, Georgia. 32 of these long range strategic reconnaissance aircraft were built by the Lockheed Skunk Works.

Lockheed SR-71A 61-7958 at Beale AFB, 28 July 1976. (U.S. Air Force)
Lockheed SR-71A 61-7958 at Beale AFB, 28 July 1976. (U.S. Air Force)

© 2015, Bryan R. Swopes

24 July 1936

Aviation, , , , , , ,
Lockheed Electra 10E NR16020 (Lockheed Martin/Purdue University Libraries, Archives and Special Collections)
Lockheed Electra 10E Special NR16020 (Lockheed Martin/Purdue University Libraries, Archives and Special Collections)

24 July 1936: On her 39th birthday, at the Union Air Terminal, Burbank, California, Amelia Earhart accepted delivery of her new Lockheed Electra 10E Special, registered NR16020.

$80,000 to buy the Electra was provided by the Purdue Research Foundation from donations made by several individuals. George Palmer Putnam, Amelia’s husband, made the arrangements to order the airplane and in March 1936 gave Lockheed the authorization to proceed, with delivery requested in June.

Amelia Earhart and her Lockeed Electra.
Amelia Earhart and her Lockeed Electra.

The Electra Model 10 was manufactured by the Lockheed Aircraft Company at Burbank, California. It was an all-metal, twin-engine, low-wing monoplane with retractable landing gear, designed as a small, medium-range airliner. In the standard configuration it carried a crew of 2 and up to 10 passengers. The Model 10 was produced in five variants with a total of 149 airplanes built between August 1934 and July 1941. Lockheed built fifteen Model 10Es. Earhart’s was serial number 1055.

Amelia Earhart in the cocpit of her Lockheed Electra 10E, NR16020.
Amelia Earhart in the cockpit of her Lockheed Electra 10E Special, NR16020. The Sperry GyroPilot is at the center of the instrument panel. (AFP/Getty Images)

Earhart’s Electra was equipped with a Western Electric Model 13C radio transmitter and Model 20B receiver for radio communication. It used a Sperry GyroPilot gyroscopic automatic pilot. Additional modifications included four auxiliary fuel tanks in the passenger compartment, a navigator’s station to the rear of that, elimination of passenger windows, installation of the autopilot, navigation equipment and additional batteries. These modifications varied from the standard airplane enough that it was restricted to carrying only members of required flight crew. This was denoted by the letter “R” in the airplane’s registration.

Amelia Earhart stands behind the additional fuel tanks installed in the aft cabin of her Electra. (AP)
Photographed from the navigator’s station at the rear of the passenger cabin, Amelia Earhart leans over the additional fuel tanks installed in her Electra. (AP)

The Electra was not ready until mid-July. Earhart first flew the new airplane on 21 July with Lockheed test pilot Elmer C. McLeod.

The Electra 10E was 38 feet, 7 inches (11.760 meters) long with a wingspan of 55 feet (16.764 meters) and overall height of 10 feet, 1 inch (3.074 meters). The standard Model 10 had and empty weight of 6,454 pounds (2,927.5 kilograms) and a gross weight of 10,500 pounds (4,762.7 kilograms). NR16020 had an empty weight of 7,265 pounds (3295.4 kilograms). Lockheed’s performance data was calculated using 16,500 pounds (7,484.3 kilograms) as the Maximum Takeoff Weight.

NR16020 had a total fuel capacity of 1,151 gallons (4,357 liters) in ten tanks in the wings and fuselage. 80 gallons (302.8 liters) of lubricating oil for the engines was carried in four tanks.

Amelia Earhart poses with her Electra's Pratt & Whitney Wasp S3H radial engine and two-bladed Hamilton Standard variable-pitch, constant-speed propeller.
Amelia Earhart poses with one of her Electra’s Pratt & Whitney Wasp S3H1 radial engines and two-bladed Hamilton Standard constant-speed propeller. (AP)

Earhart’s Electra 10E Special was powered by two air-cooled, supercharged, 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp S3H1 nine-cylinder radial engines, with a compression ratio of 6:1. These engines used a single-stage centrifugal supercharger and were rated at 550 horsepower at 2,200 r.p.m. at 5,000 feet (1,524 meters) and 600 horsepower at 2,250 r.p.m. for take off. The direct-drive engines turned 9 foot, 7/8-inch (3.010 meters) diameter, two-bladed, Hamilton Standard variable-pitch, constant-speed propellers. The Wasp S3H1 is 4 feet, 3.60 inches (1.311 meters) in diameter and 3 feet, 7.01 inches (1.093 meters) long. It weighed 865 pounds (392 kilograms).

Clarence L. (“Kelly”) Johnson with Amelia Earhart. (Lockheed Martin)

The maximum speed for the Model 10E Special at Sea Level and maximum takeoff weight was 177 miles per hour (285 kilometers per hour), a reduction of 25 miles per hour (40 kilometers per hour) over the standard airplane. The maximum range was calculated to be 4,500 miles (7,242 kilometers)

Lockheed test pilot Elmer C. McCleod with a Lockheed Model 10 Electra, "Phantom of the Sky." (Lockheed Martin via dmairfield.com)
Lockheed test pilot Elmer C. McCleod with a Lockheed Model 10 Electra, “Phantom of the Sky.” (Lockheed Martin via dmairfield.com)

© 2017, Bryan R. Swopes

22 July 1933

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Wiley Hardeman Post, 1898–1935. (Underwood & Underwood)

22 July 1933: At 11:50½ p.m., Wiley Hardeman Post and his Lockheed Model 5C Vega, NR105W, The Winnie Mae of Oklahoma, landed at Floyd Bennett Field, Long Island, New York.

Post had departed from there on 15 July and in 7 days, 18 hours, 49½ minutes, he flew 15,596 miles (25,099.3 kilometers), circling the Northern Hemisphere. He made 11 stops for fuel and rest, and had one minor accident which required repairs to the airplane. (Note the Standard propeller clearly visible in the photograph below.)

In 1931, he had flown approximately the same route, with a navigator, Harold Gatty, aboard. For this flight Post was by himself.

This was the first solo around-the-world flight. Wiley Post was the first pilot to have flown around the world twice.

Wiley Post climbs out of the cockpit of his Lockheed Vega monoplane, Winnie Mae, after completing the first solo flight around the world at Floyd Bennet Field, Long Island, N.Y., midnight, July 22, 1933. Wiley set a new record with the distance of 15,596 miles, 25,099 kilometer, in 7 days, 18 hours, 49 minutes. (AP Photo)
“Wiley Post climbs out of the cockpit of his Lockheed Vega monoplane, Winnie Mae, after completing the first solo flight around the world at Floyd Bennett Field, Long Island, N.Y., midnight, July 22, 1933. Wiley set a new record with the distance of 15,596 miles, 25,099 kilometer, in 7 days, 18 hours, 49 minutes.” (AP Photo)

The Vega was a single-engine, high-wing monoplane was designed by John Knudsen (“Jack”) Northrop and Gerrard Vultee. It was a very state-of-the-art aircraft for its time. It used a streamlined monocoque fuselage made of spiral strips of vertical grain spruce pressed into concrete molds and held together with glue. The wing and tail surfaces were fully cantilevered, requiring no bracing wires or struts to support them.

The techniques used to build the Vega were very influential in aircraft design. It also began Lockheed’s tradition of naming its airplanes after stars and other astronomical objects.

The Winnie Mae was built by Lockheed Aircraft Company at Burbank, California in 1930 as a Model 5B Vega, serial number 122. It was purchased by an Oklahoma oil driller, Florence C. (“F.C.”) Hall, on 21 June 1930, and named for his daughter, Winnie Mae Hall, The Winnie Mae of Oklahoma. The new airplane was painted white with purple trim. In 1932, NC105W was modified to the Vega 5C standard.

The Lockheed Model 5C Vega is 27 feet, 6 inches (8.382 meters) long with a wingspan of 41 feet (12.497 meters) and overall height of 8 feet, 2 inches (2.489 meters). Its empty weight is 2,595 pounds (1,177 kilograms) and gross weight is 4,500 pounds (2,041 kilograms).

Winnie Mae was powered by an air-cooled, supercharged 1,343.80-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp C, serial number 3088, a single-row, nine cylinder, direct-drive radial engine. The Wasp C was rated at 420 horsepower at 2,000 r.p.m. at Sea Level. It was 3 feet, 6.63 inches (1.083 meters) long with a diameter of 4 feet, 3.44 inches (1.307 meters) and weighed 745 pounds (338 kilograms).

The standard Model 5C had a cruise speed of 165 miles per hour (266 kilometers per hour) and maximum speed of 185 miles per hour (298 kilometers per hour). The service ceiling was 15,000 feet (4,570 meters) and range in standard configuration was 725 miles (1,167 kilometers).

An estimated 50,000 spectators greet Wiley Post on his return to Floyd Bennett Field, 22 July 1933. Post is visible jut behind the trailing edge of the Vega's left wing. (Unattributed)
An estimated 50,000 spectators greeted Wiley Post on his return to Floyd Bennett Field, 22 July 1933. Post is visible just behind the trailing edge of the Vega’s left elevator. (Unattributed)

Wiley Post flew the Winnie Mae for F.C. Hall, and flew it around the world in 1931 with Harold Gatty as navigator. Post used it to set several speed records and to compete in the National Air Races. Post purchased the airplane from Hall, 8 July 1931.

When the Vega and its Wasp engine had reached 745 hours of operation, they were  overhauled by Braniff Airways at Oklahoma City, Oklahoma. The Wasp C was modified with cylinders from a Wasp C1. This increased the compression ratio from 5.25:1 to 6.0:1. Using 87-octane aviation gasoline, it could produce 500 horsepower at 2,200 r.p.m. (5-minute limit). The airplane’s original two-bladed Standard fixed-pitch steel propeller was later replaced by a Smith 450-SI controllable-pitch propeller with Pittsburgh Screw and Bolt hollow steel blades.

Among other modifications, Post had the wing’s angle of incidence decreased 10° which increased the Vega’s speed by 10 miles per hour (16 kilometers per hour). The fixed tail skid was shortened to allow the airplane to reach a higher angle of attack for takeoff and landing. For the 1933 around-the-world flight, six auxiliary tanks were installed in the fuselage, giving the Vega a total fuel capacity of 645 gallons (2,442 liters). It was also equipped with a Sperry gyroscopic autopilot.

These modification required the Vega to be licensed in a restricted category, and it was re-registered NR105W.

After Wiley Post was killed in an airplane crash near Barrow, Alaska, 15 August 1935, his widow, Mae Laine Post, sold NR105W to the Smithsonian Institution. It is on display in the Time and Navigation Exhibition at the National Air and Space Museum, Washington, D.C.

Wiley Post’s Lockheed Model 5C Vega, NR105W, Winnie Mae of Oklahoma, at the National Air and Space Museum. (Photo by Dane Penland, National Air and Space Museum, Smithsonian Institution)

© 2016, Bryan R. Swopes