Major Marion E. Carl, USMC, with a Douglas D-558-I Skystreak at Muroc Dry Lake, 1947. (U.S. Navy)
25 August 1947: Major Marion Eugene Carl, United States Marine Corps, flying the Douglas D-558-I Skystreak, Bu. No. 37970, set a new Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Straight Course, averaging 1,047.356 kilometers per hour (650.797 miles per hour).¹ The Skystreak was flown over a course laid out on Muroc Dry Lake, site of Muroc Army Air Field (now Edwards Air Force Base) in the high desert of Southern California.
Douglas D-558-I Skystreak Bu. No. 37970 makes a pass over the 3 kilometer course on Muroc Dry Lake. (U.S. Navy)
Four passes were made over the course at an altitude of 200 feet (61 meters) or lower. Two runs were made in each direction to compensate for any head or tail winds. The official speed for a record attempt was the average of the two best consecutive passes out of the four.
Major Carl’s record exceeded one set by Commander Turner F. Caldwell, Jr., U.S. Navy, just five days earlier by 10.053 miles per hour (16.178 kilometers per hour).
Major Marion E. Carl, USMC, and Commander Turner F. Caldwell, Jr., USN, stand with the record-setting Douglas D-558-I Skystreak, Bu. No. 37970, on Muroc Dry Lake. (U.S. Navy)
The D-558 Program was intended as a three phase test program for the U.S. Navy and the National Advisory Committee on Aeronautics (NACA) to investigate transonic and supersonic flight using straight and swept wing aircraft powered by turbojet and/or rocket engines. The Douglas Aircraft Company designed and built three D-558-I Skystreaks and three D-558-II Skyrockets. The Phase I aircraft were flown by Douglas test pilot Eugene Francis (“Gene”) May, Navy Project Officer Commander Turner F. Caldwell, Jr., and Major Marion Carl.
Major Marion E. Carl, USMC; Gene May, Douglas Aircraft Company; Commander Turner F. Caldwell, USN.
The D-558-I Skystreak (also referred to as the D-558-1) was a single-engine, straight winged, turbojet-powered airplane. It was built of magnesium and aluminum for light weight, but was designed to withstand very high acceleration loads. It was 35 feet, 8 inches (10.871 meters) long with a wingspan of 25 feet, 0 inches (7.62 meters) and overall height of 12 feet, 1¾ inches (3.702 meters). The airplane had retractable tricycle landing gear. Its empty weight was approximately 7,500 pounds (3,400 kilograms), landing weight at the conclusion of a flight test was 7,711 pounds (3,498 kilograms). The maximum takeoff weight was 10,105 pounds (4,583.6 kilograms). The aircraft fuel load was 230 gallons (870.7 liters) of kerosene.
The D-558-I was powered by a single Allison J35-A-11 turbojet engine. The J35 was a single-spool, axial-flow turbojet with an 11-stage compressor section, 8 combustion chambers and single-stage turbine. The J35-A-11 was rated at 5,000 pounds of thrust (22.24 kilonewtons). The engine was 12 feet, 1.0 inches (3.683 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,455 pounds (1,114 kilograms). The J35-A-11 was a production version of the General Electric TG-180, initially produced by Chevrolet as the J35-C-3. It was the first widely-used American jet engine.
The D-558-I had a designed service ceiling of 45,700 feet (13,930 meters). Intended for experimental flights of short duration, it had a very short range and took off and landed from the dry lake at Muroc. (After 1949, this would be known as Edwards Air Force Base.) The experimental airplane was not as fast as the more widely known Bell X-1 rocketplane, but rendered valuable research time in the high transonic range.
Gene May did reach Mach 1.0 in 37970, 29 September 1948, though he was in a 35° dive. This was the highest speed that had been reached up to that time by an airplane capable of taking off and landing under its own power.
The three D-558-I Skystreaks made a total of 229 flights and Bu. No. 37970 made 101 of them. After the Douglas test program was completed, -970 was turned over to NACA as NACA 140, but it was quickly grounded after the crash of the number two aircraft, and was used for spare parts for number three.
Today, 37970 is in the collection of the National Naval Aviation Museum at Naval Air Station Pensacola, Florida. The other surviving Skystreak, Bu. No. 37972, is at the Carolinas Aviation Museum, Charlotte-Douglas International Airport, Charlotte, North Carolina.
This painting depicts Major Marion E. Carl’s speed record attempt over the 3 kilometer course at Muroc Dry Lake. (Steve Cox, 24″ × 30″, acrylic on board)
For biographical information about Marion Carl, please see “This Day in Aviation” for 24 August 1942 at: https://www.thisdayinaviation.com/24-august-1942/
Amelia Earhart with her Lockheed Vega after her record-setting solo nonstop flight across North America, 25 August 1932. (Encyclopedia Britannica)
24–25 August 1932: Amelia Earhart flew her Lockheed Model 5B Vega, NR7952, from Los Angeles, California, to Newark, New Jersey, a distance of 3,939.25 kilometers (2,447.74 miles), in 19 hours, 5 minutes. She had departed Los Angeles Municipal Airport (now known as LAX) at 7:26:54 p.m. Pacific Time, 24 August, and landed at Newark Municipal Airport at 11:30 a.m. Eastern Time the following day. This set a Fédération Aéronautique Internationale (FAI) women’s World Record for Distance in a Straight Line Without Landing.¹ Her average speed for the flight was 206.42 kilometers per hour (128.27 miles per hour).
National Aeronautics Association Certificate of Record, issued on behalf of the Fédération Aéronautique Internationale.
Amelia Earhart was the first woman to fly solo coast-to-coast. Less than a year later, she would break her own record by almost two hours.
A small crowd gathers around Amelia Earhart and her Lockheed Model 5B Vega at Newark Municipal Airport, 25 August 1932. (AP)
Built by the Lockheed Aircraft Company, the Model 5 Vega was a single-engine high-wing monoplane. The fuselage was molded wood monocoque construction and the wing was cantilevered wood. The Vega 5B 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 1,650 pounds (748.4 kilograms) and gross weight is 4,375 pounds (1,985 kilograms).
Aircraft Registration Certificate, Lockheed Vega 5B, serial number 22, NC7952.
Earhart’s modified Vega 5B is powered by an air-cooled, supercharged 1,343.804-cubic-inch-displacement (22.021 liter) Pratt & Whitney Wasp C nine cylinder radial engine. The Wasp C was rated at 420 horsepower at 2,000 r.p.m. at Sea Level.² It was 3 feet, 6.63 inches (1.083 meters) long, 4 feet, 3.44 inches (1.307 meters) in diameter, and weighed 745 pounds (338 kilograms). It drove a two-bladed Hamilton Standard controllable-pitch propeller through direct drive.
Just three months earlier, Earhart had flown solo across the Atlantic Ocean in this same airplane, which she called her “Little Red Bus.” Today, Lockheed Vega NR7952 is in the collection of the Smithsonian Institution National Air and Space Museum.
Amelia Earhart’s Lockheed Model 5B Vega, NR7952, at the Smithsonian Institution National Air and Space Museum. (NASM)
¹ FAI Record File Number 12342
² The Pratt & Whitney Wasp C was also used by the U.S. Army and Navy, designated R-1340-7. In military service, it was rated at 450 horsepower at 2,100 r.p.m. at Sea Level.
Jackie Cochran with her record-setting Northrop T-38A-30-NO Talon, 60-0551, at Edwards Air Force Base, California, 1961.
24 August 1961: At Edwards Air Force Base, California, Jacqueline Cochran flew a Northrop/Ryan Aeronautical T-38A-30-NO Talon, 60-0551, to an average speed of 1,358.6 kilometers per hour (844.2 miles per hour) over a straight 15-to-25 kilometer course, setting a Fédération Aéronautique Internationale (FAI) world speed record for women.¹
Jackie Cochran’s FAI record certificate in the San Diego Air and Space Museum Archives. (Bryan R. Swopes)
“August 24 Big day! First solo in production. Jackie took off in Northrop T-38 for 15–25 record attempt at 9:00 am. I chased in F-100. Flew good pattern and lit afterburners 50 miles from west outer marker. Jackie held good altitude through trap and made a good procedure turn. Lit afterburner 40 miles out on return run and nailed the altitude down perfect. Average speed was 844 mph. All the officials were pleased and the record was confirmed. One down and nine to go.”
— 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, Pages 301–302.
Jackie Cochran and Colonel Chuck Yeager at Edwards Air Force Base, California, after a flight in the record-setting Northrop T-38A Talon. (U.S. Air Force)
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, 11 inches (3.937 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 60-0551 at Edwards Air Force Base, 1961. (FAI)
Captain Marion E. Carl, USMC, with a Grumman F4F-3 Wildcat. (U.S. Navy)
24 August 1942: Flying a Grumman F4F Wildcat, Lieutenant Marion Eugene Carl, United States Marine Corps, a 27-year-old fighter pilot assigned to Marine Fighter Squadron 223 (VMF-223) based at Henderson Field, Guadalcanal Island, shot down four enemy airplanes in one day. They were a Mitsubishi A6M “Zeke” fighter, a Mitsubishi G4M1 “Betty” medium bomber and two Nakajima B5N2 “Kate” torpedo bombers. Carl had previously shot down an A6M during the Battle of Midway, less than three months earlier. He now had five aerial combat victories, making him the Marine Corps’ first ace.
Captain Carl was awarded the Navy Cross (his second) for his actions in the Solomon Islands from 24 August to 9 September 1942.
Marion Carl’s fighter was a Grumman F4F-4 Wildcat, designed by Robert Leicester Hall as a carrier-based fighter for the United States Navy. The F4F-4 was a single-place, single-engine, mid-wing monoplane with retractable landing gear.
Grumman F4F-4 Wildcat. (U.S. Navy)
The F4F-4 was 29 feet, 9-3/8 inches (9.077 meters) long, with a wingspan of 38 feet, 0 inches (11.582 meters) and overall height of 12 feet, 1-3/8 inches (3.693 meters). Unlike the preceding F4F-3, the F4F-4 had folding wings for storage aboard aircraft carriers. With the wings folded, the airplane was 14 feet, 4 inches (4.369 meters) wide. Its empty weight was 5,895 pounds (2,674 kilograms), and the gross weight was 7,975 pounds (3,617 kilograms).
The F4F-4 was powered by an air-cooled, supercharged, 1,829.39-cubic-inch-displacement (29.978 liter) Pratt & Whitney Twin Wasp SSC7-G (R-1830-86) two-row, 14-cylinder radial engine with a compression ratio of 6.7:1. The R-1830-86 had a normal power rating of 1,100 at 2,550 r.p.m., from Sea Level to 3,300 feet (1,006 meters), and 1,000 horsepower at 2,550 r.p.m. at 19,000 feet (5,791 meters). It was rated at 1,200 horsepower at 2,700 r.p.m. for takeoff. The engine turned a three-bladed Curtiss Electric propeller with a diameter of 9 feet, 9 inches (2.972 meters) through a 3:2 gear reduction. The R-1830-86 was 4 feet, 0.19 inches (1.224 meters) in diameter, 5 feet, 7.44 inches (1.713 meters) long, and weighed 1,560 pounds (708 kilograms).
The F4F-4 had a maximum speed of 284 miles per hour (457 kilometers per hour) at Sea Level, and 320 miles per hour (515 kilometers per hour) at 18,800 feet (5,730 meters). Its service ceiling was 34,000 feet (10,363 meters).
Grumman F4F-3 Wildcat in three-color camouflage
While the F4F-3 Wildcat was armed with four air-cooled Browning AN-M2 .50-caliber machine guns; the F4F-4 had six. It carried 1,400 rounds of ammunition.
The prototype XF4F-1 made its first flight in 1935. It was substantially improved as the XF4F-2. The first production F4F-3 Wildcat was built in February 1940. The airplane remained in production through World War II, with 7,860 built by Grumman and General Motors Eastern Aircraft Division (FM-1 Wildcat).
According to the National Naval Aviation Museum, F4F Wildcats held a 9:1 ratio of victories over Japanese aircraft, with 1,006 enemy airplanes destroyed in combat.
A Grumman F4F Wildcat at Henderson Field, Guadalcanal. There are 19 Japanese flags painted on the fuselage, suggesting that this is Major John L. Smith’s fighter. (U.S. Navy)
Marion Eugene Carl was born at Hubbard, Oregon, 1 November 1915. He was the second of four children of Herman Lee Carl, a dairy farmer, and Ellen Lavine Ellingsen Carl.
Carl graduated from Oregon State College at Corvallis, Oregon, and was commissioned as a second lieutenant in the United States Army Reserve, 31 May 1938. Lieutenant Carl soon resigned this commission to accept an appointment as an Aviation Cadet, United States Navy. He enlisted as a private, first class, Volunteer Marine Corps Reserve, 17 July 1938, and was designated a student Enlisted Naval Aviation Pilot assigned to the Naval Reserve Aviation Base, Squantum, Massachusetts. He entered flight school as an Aviation Cadet at Naval Air Station Pensacola near Pensacola, Florida, 26 July 1938.
Lieutenant Marion E. Carl, USMC, Naval Aviator. (U.S. Navy)
After completing flight training, Carl was commissioned as a Second Lieutenant, United States Marine Corps Reserve, 20 October 1939. He was then assigned to Marine Fighting Squadron One (VMF-1) at Brown Field, Quantico, Virginia.
In 1940, Lieutenant Carl returned to NAS Pensacola as a flight instructor. On 25 February 1941, Second Lieutenant Carl, U.S.M.C.R., was appointed a Second Lieutenant, United States Marine Corps.
Lieutenant Carl was transferred to VMF-221 at San Diego, California, as a fighter pilot. The unit was assigned to the aircraft carrier USS Saratoga (CV-3) for transportation to Marine Corps Air Station Ewa, Oahu, Territory of Hawaii. On 25 December 1941, VMF-221 was deployed to Midway Atoll.
Marion Carl and his squadron fought during the Battle of Midway. Flying a Grumman F4F-3 Wildcat, Bu. No. 1864,¹ on 4 June 1942, he shot down his first enemy airplane, a Mitsubishi A6M Zero fighter, and damaged two others. Lieutenant Carl was awarded the Navy Cross for his actions in that decisive battle.
Marion Carl was next assigned to VMF-223 under the command of Captain John L. Smith. The Marine fighter squadron was the first air unit to arrive at Henderson Field on the island of Guadalcanal in the Solomons, 20 August 1942. This was a critical airfield, originally built by the Japanese military but occupied by Allied forces. On 24 August, Lieutenant Carl became the Marine Corps’ first “ace.”
Carl was shot down in 9 September 1942 and was missing for five days. He was helped by islanders who eventually returned him to his base.
The squadron departed Guadalcanal 16 October 1942, and sailed to San Francisco, California. VMF-223 was credited with destroying 110½ enemy aircraft. Carl was credited with 16.
Lieutenant Carl married Miss Edna T. Kirvin at New York City, New York, 7 January 1943.
On 26 January, he took command of VMF-223. On 8 May 1943, Lieutenant Carl was promoted to the temporary rank of captain. The squadron was re-equipped with the new Vought-Sikorsky F4U-1 Corsair. Training in the new fighter took place at MCAS El Toro, in southern California.
In August, the squadron returned to combat in the Solomons. By the end of 1943, Major Carl’s total of enemy aircraft destroyed was 18½ with 3 damaged, making him the seventh highest-scoring Marine fighter pilot of World War II.
Major Marion E. Carl, USMC, commanding VMF-223 in 1943. The aircraft is a Vought F4U Corsair in which Carl shot down two enemy aircraft in December 1943. (U.S. Navy)
After the War Marion Carl was assigned as a test pilot at NAS Patuxent River, Maryland, testing jet aircraft on aircraft carriers. He was also the first Marine Corps pilot to fly a helicopter. Carl commanded the Marine’s first jet squadron, VMF-122, which flew the McDonnell FH-1 Phantom. He was promoted to lieutenant colonel 7 August 1947.
In May 1955, Colonel Carl commanded Marine Photo Reconnaissance Squadron One (VMJ-1). The squadron flew the McDonnell FH-2 Banshee from air bases on the island of Formosa (Taiwan) on secret missions over the People’s Republic of China.
At Muroc Army Air Field (now Edwards Air Force Base) Marion Carl tested the Douglas D-558-I Skystreak and D-558-II Skyrocket, setting world records for speed and altitude. He was promoted to colonel, 1 October 1956.
Major Marion E. Carl, USMC, and Commander Turner F. Caldwell, Jr., USN, stand with the record-setting Douglas D-558-I Skystreak, Bu. No. 37970, on Muroc Dry Lake. (U.S. Navy)
By 1962 Colonel Carl was Director of Marine Corps Aviation. He was promoted to brigadier general, 1 June 1964. He commanded the First Marine Brigade during the Vietnam War and flew combat missions in jet fighters and helicopter gun ships.
Major General Marion E. Carl, United States Marine Corps.
Carl was promoted to major general in August 1967, with his date of rank retroactive to 1 June 1964. Carl commanded the 2nd Marine Aircraft Wing, then served as Inspector General of the Marine Corps from 1970 until 1973. When he retired in 1973, General Carl had accumulated more that 13,000 flight hours.
During his military career, Major General Carl was awarded the Navy Cross with two gold stars (three awards); The Legion of Merit with valor device and three gold stars (four awards); The Distinguished Flying Cross with four gold stars (five awards); and the Air Medal with two gold and two silver stars (twelve awards).
Tragically, General Carl was murdered in Roseburg, Oregon, 28 June 1998, as he defended his wife, Edna, during a home-invasion robbery. Mrs. Carl was wounded, but survived.
Major General Marion E. Carl, United States Marine Corps, is buried at Arlington National Cemetery.
Semper fidelis
A Mitsubishi A6M2 Type 0 Model 21 “Zero” fighter takes off from an aircraft carrier of the Imperial Japanese Navy. Marion Carl shot down one of these and damaged two others during the Battle of Midway, 4 June 1942. (Imperial Japanese Navy)Mitsubishi A6M3 Type 0 Model 22 “Zeke” in the Solomon Islands, 1943. (This fighter is flown by Petty Officer 1st Class Hiroyoshi Nishizawa, one of the most successful fighter pilots of World War II.) (Imperial Japanese Navy)A Mitsubishi G4M1 Type 1 Model 11 “Betty” takes off from Rabaul, 1942.Nakajima B5N2 Type 97 “Kate”. Marion Carl shot down two of these torpedo bombers, 24 August 1942.
¹ The fighter flown by Marion Carl to shoot down his first enemy airplane is often cited as Grumman F4F-3 Bu. No. 4000 (second bureau number series, 1935–1940). However, the entry in Carl’s certified pilot logbook for 4 June 1942 states the airplane he flew was F4F-3 Bu. No. 1864.
The first prototype Lockheed YC-130 Hercules, 53-3397, takes of from the Lockheed Air Terminal, Burbank, California, 23 August 1954. (Lockheed Martin)
23 August 1954: The first of two Lockheed YC-130 Hercules four-engine transport prototypes, 53-3397, made its first flight from the Lockheed Air Terminal at Burbank, California, to Edwards Air Force Base. The flight crew consisted of test pilots Stanley Beltz and Roy Wimmer, with Jack G. Real (a future Lockheed vice president) and Dick Stanton as flight engineers. From a standing start, the YC-130 was airborne in 855 feet (261 meters), The flight lasted 1 hour, 1 minute.
The C-130 was designed as a basic tactical transport, capable of carrying 72 soldiers or 64 paratroopers. All production aircraft have been built at Lockheed Martin’s Marietta, Georgia, plant.
Lockheed YC-130 53-3397 during its first flight, 23 August 1954. (Lockheed Martin)
The first production model, the C-130A Hercules, was flown 7 April 1955. It was 97.8 feet (29.81 meters) long with a wingspan of 132.6 feet (40.42 meters), and height of 38.1 feet (11.61 meters). Total wing area was 1,745.5 square feet (162.16 square meters). The transport’s empty weight was 59,164 pounds (26,836 kilograms) and takeoff weight, 122,245 pounds (55,449 kilograms).
The C 130 has a rear loading ramp for vehicles, and there is a large cargo door on the left side of the fuselage, forward of the wing, The transport’s cargo compartment volume is 3,708 cubic feet (105.0 cubic meters). It could carry 35,000 pounds (15,876 kilograms) of cargo.
Lockheed YC-130 53-3397 during its first flight, 23 August 1954. (Lockheed Martin)
The C-130A was equipped with four Allison T56-A-1A turboshaft engines, driving three-bladed propellers. The engines produced 3,094 shaft horsepower at 13,820 r.p.m. (continuous), and 3,460 horsepower, Military Power (30-minute limit) or Takeoff ( 5-minute limit).
The C-130A had a cruise speed of 286 knots (329 miles per hour/530 kilometers per hour) and maximum speed of 326 knots (375 miles per hour/604 kilometers per hour) at 24,200 feet (7,376 meters). Its range with a 35,000 pound ( kilogram) payload was 1,835 nautical miles (2,112 statute miles/3,398 kilometers). The initial rate of climb at Sea Level was 4,320 feet per minute (21.95 meters per second). The combat ceiling was 38,700 feet (11,796 meters).
Lockheed YC-130 Hercules prototype, 53-3397. (SDA&SM)Lockheed C-130A-LM Hercules 55-031, circa 1957. The radome has been added and the tip of the vertical fin squared off. (U.S. Air Force)
In addition to its basic role as a transport, the C-130 has also been used as an aerial tanker, a command-and-control aircraft, weather reconnaissance, search and rescue and tactical gunship. It has even been used as a bomber, carrying huge “Daisy Cutters” to clear large areas of jungle for use as helicopter landing zones, or, more recently, the Massive Ordnance Air Blast “mother of all bombs.” The aircraft has been so versatile that it has served in every type of mission. Over 40 variants have been built by Lockheed, including civilian transports. It is in service worldwide.
The latest version is the Lockheed C-130J Hercules. After 70 years, the C-130 is still in production, longer than any other aircraft type.
YC-130 53-3397 was scrapped at Indianapolis in 1962.
Lockheed C-130J Hercules transports under construction at Lockheed Martin’s Marietta, Georgia plant. (Lockheed Martin)
