At 12:20 UTC, 15 July 1975, Soyuz 19 launched from Gagarin’s Start at Baikonur Cosmosdrome, Kazakh SSR with Alexei Leonov and Valeri Kubasov, both on their second space flights. The launch vehicle was a Soyuz-U three-stage rocket.
At 19:50 UTC, 15 July 1975, Apollo ASTP lifted off from Launch Complex 39A, Kennedy Space Center, Cape Canaveral, Florida. The crew was Thomas P. Stafford on his fourth space flight, Vance D. Brand on his first, and Donald K. “Deke” Slayton also on his first. The launch vehicle was a Saturn IB.
At 16:19:09 UTC, 17 July 1975, the two orbiting spacecraft rendezvoused in orbit and docked. Using a Docking Module airlock, the two crews each opened their spacecraft hatches and shook hands. The two ships remained joined for 44 hours, separating once for the Soyuz crew to take its turn to maneuver for docking with the Apollo Command and Service Module.
The Apollo command module from the mission is on display at the California Science Center in Los Angeles. The descent module of Soyuz 19 is on display at the RKK Energiya museum in Korolyov, Moscow Oblast, Russia.
This was the final flight of the Apollo spacecraft.
17 July 1965: At Air Force Plant 42, Palmdale, California, the second North American Aviation B-70 Valkyrie prototype, XB-70A-2-NA 62-0207, took off on its maiden flight enroute Edwards Air Force Base where it would continue the flight test program with its sister ship.
The Valkyrie was designed as a Mach 3+ strategic bomber, capable of flight above 70,000 feet (21,336 meters), with intercontinental range. It’s altitude allowed it to avoid interceptors of the time, but improvements in radar-guided surface-to-air missiles increased its vulnerability. Ultimately, though, political decisions ended the B-70 program.
62-0207 was flown just 46 times, for a total of 92 hours, 22 minutes of flight. Changes to the aircraft corrected the deficiencies discovered in testing the Number 1 XB-70A, 62,-201. The most visible change was 5° dihedral added to the wings for improved stability. On 16 April 1966, 62-0207 reached its maximum design speed, Mach 3.08, which it sustained for 20 minutes.
Less than one year after its first flight, 8 June 1966, the Valkyrie was involved in a mid-air collision with a Lockheed F-104N and crashed just north of Barstow, California. North American’s B-70 test pilot, Al White, was seriously injured and co-pilot, Major Carl Cross, USAF, was killed. NASA test pilot Joe Walker, flying the F-104, was also killed.
17 July 1962: At 9:31:10.0 a.m., the Number 3 North American Aviation X-15, 56-6672, was airdropped from a Boeing NB-52A Stratofortress, 52-003, over Delamar Dry Lake, Nevada. Air Force project test pilot Major Robert M. (“Bob”) White was in the cockpit. This was the 62nd flight of the X-15 Program, and Bob White was making his 15th flight in an X-15 hypersonic research rocketplane. The purpose of this flight was to verify the performance of the Honeywell MH-96 flight control system which had been installed in the Number 3 ship. Just one minute before drop, the MH-96 failed, but White reset his circuit breakers and it came back on line.
After dropping from the B-52’s wing, White fired the X-15’s Reaction Motors XLR-99 rocket engine and began to accelerate and climb. The planned burn time for the 57,000-pound-thrust engine was 80.0 seconds. It shut down 2 seconds late, driving the X-15 well beyond the planned peak altitude for this flight. Instead of reaching 280,000 feet (85,344 meters), Robert White reached 314,750 feet (95,936 meters). This was an altitude gain of 82,190 meters (269,652 feet), which was a new Fédération Aéronautique Internationale (FAI) world record.¹ The rocketplane reached Mach 5.45, 3,832 miles per hour (6,167 kilometers per hour).
Because of the increased speed and altitude, White was in danger of overshooting his landing at Edwards Air Force Base in California. He passed over the north end of Rogers Dry Lake and crossed the “high key”—the point where the X-15 landing maneuver begins—too high and too fast at Mach 3.5 at 80,000 feet (24,384 meters). Without power, White made a wide 360° turn over Rosamond Dry Lake then came back over the high key at a more normal 28,000 feet (8,534.4 meters) and subsonic speed. He glided to a perfect touch down, 10 minutes, 20.7 seconds after being dropped from the B-52.
This was the first time that a manned aircraft had gone higher than 300,000 feet (91,440 meters). It was also the first flight above 50 miles. For that achievement, Bob White became the first X-15 pilot to be awarded U.S. Air Force astronaut wings. His 314,750-foot altitude (95,936 meters) also established a Fédération Aéronautique Internationale (FAI) world altitude record, which will probably never be broken. To qualify, a new record would have to exceed White’s altitude by at least 3%, or more than 324,419 feet (98,882.9 meters). As the FAI-recognized boundary of Space is 328,083.99 feet (100,000 meters), any prospective challenger would have to hit a very narrow band of the atmosphere.
Major White had been the first pilot to fly faster than Mach 4, Mach 5 and Mach 6. He was the first to fly over 200,000 feet, then over 300,000 feet. He was a graduate of the Air Force Experimental Test Pilot School and flew tests of many aircraft at Edwards before entering the X-15 program. He made at total of sixteen X-15 flights.
A P-51 Mustang fighter pilot with the 355th Fighter Group in World War II, he was shot down by ground fire on his fifty-third combat mission, 23 February 1945, and captured. He was held as a prisoner of war until the war in Europe came to an end in April 1945.
After the war, White accepted a reserve commission while he attended college to earn a degree in engineering. He was recalled to active duty during the Korean War, and assigned to a P-51 fighter squadron in South Korea. Later, he commanded the 22nd Tactical Fighter Squadron (flying the Republic F-105 Thunderchief supersonic fighter bomber) based in Germany, and later, the 53rd TFS. During the Vietnam War, Lieutenant Colonel White, as the deputy commander for operations of the 355th Tactical Fighter Wing, flew seventy combat missions over North Vietnam in the F-105D, including leading the attack against the Paul Doumer Bridge at Hanoi, 11 August 1967, for which he was awarded the Air Force Cross.
He next went to Wright-Patterson AFB where he was director of the F-15 Eagle fighter program. In 1970 he returned to Edwards AFB as commander of the Air Force Flight Test Center. White was promoted to Major General in 1975.
General White retired from the U.S. Air Force in 1981. He died 10 March 2010.
17 July 1938: For more than ten years it had been Clyde Groce Corrigan’s ambition to emulate his hero, Charles A. Lindbergh, and to fly solo, non-stop across the Atlantic Ocean. An aircraft mechanic, he had worked on the construction of the Spirit of St. Louis as an employee of Ryan Aircraft Co. in San Diego, California.
Corrigan had assumed the first name “Douglas,” possibly out of admiration for “The King of Hollywood,” actor Douglas Fairbanks.
In 1933, Corrigan and his younger brother Harry Groce Corrigan, an aeronautical engineer, bought a 1929 Curtiss Model 50 Robin B, a single-engine, high-wing monoplane. The Robin was 25 feet, 8½ inches (7.836 meters) long with a wingspan of 41 feet (12.497 meters) and height of 7 feet, 9½ inches (2.375 meters). In standard configuration, the Robin weighed 1,472 pounds (667.7 kilograms) empty, and 2,440 pounds (1,106.8 kilograms) loaded. Its cruise speed was 84 miles per hour (135 kilometers per hour) and the maximum speed was 100 miles per hour (161 kilometers per hour). The range was 480 miles (773 kilometers).
Corrigan continuously worked on the airplane, repairing, overhauling, re-skinning, modifying. He replaced the Robin’s original water-cooled 502.65-cubic-inch-displacement (8.237 liter) Curtiss OX-5 V-8 engine (rated at 90 horsepower at 1,400 r.p.m.) with a more modern, more powerful, Wright “J-6-5.” This engine was an air-cooled, supercharged, 539.96-cubic-inch-displacement (8.848 liter) Wright R-540 Whirlwind 150 single-row 5-cylinder radial which produced 150 horsepower at 1,800 r.p.m. The direct-drive engine turned a two-bladed propeller. In this configuration, the airplane was a Robin J-1 (Curtiss Model 50H)He also installed extra fuel tanks. The Whirlwind 150 was 3 feet, 51.1 inches (1.044 meters) long, 3 feet, 9.0 inches (1.143 meters) in diameter, and weighed 370 pounds (168 kilograms).
The Bureau of Commerce had repeatedly refused to authorize Corrigan’s requests to make a trans-Atlantic flight as his airplane was considered unsuitable for such a flight. He decided to go anyway.
In early July 1938, Douglas Corrigan made a non-stop flight from Long Beach, California to Floyd Bennett Field, Brooklyn, New York. He announced that he would make the return flight and had his Robin fueled with a total of 320 gallons (1,211.3 liters) of gasoline.
At 5:15 a.m., 17 July 1938, Corrigan and his Robin took off from Floyd Bennett Field and disappeared into a cloudy sky. 28 hours, 13 minutes later, he landed at Baldonnell Aerodrome (now known as Casement Aerodrome), County Dublin, Ireland.
He said that he had become disoriented in the clouds, misread his compass and flew East rather than West. He was forever after known as “Wrong Way” Corrigan.
Corrigan’s Curtiss Robin was disassembled and returned to the United States aboard ship. The airplane as placed in storage at his home in southern California. In 1988, the airframe and components were transported to Hawthorne Airport (HHR), at Hawthorne, California, where the airplane was reassembled and placed on display. The current status of NX9243 is not known. Original records of NX9243 from the Aeronautics Branch, Department of Commerce, are in the collection of the Smithsonian Institution National Air and Space Museum.
Clyde Groce Corrigan¹ was born 22 January 1907 at Galveston, Texas. He was the first of three children of Clyde Sinclair Corrigan, a civil engineer, and Evelyn Groce Nelson Corrigan, a school teacher.
Corrigan began flight instruction in 1924, flying a Curtiss “Jenny” at Grand Central Air Terminal in Glendale, California. Lessons were expensive and his training took time. He first soloed 25 March 1926.
In 1927, Corrigan was employed by B.F. Mahoney Aircraft at San Diego, California. This soon became the Ryan Airlines Company. Corrigan is reported to have worked on the construction of Charles A. Lindbergh’s Spirit of St. Louis.
Douglas Corrigan wrote his autobiography, That’s My Story, which was published 1 January 1938 by E.P. Dutton & Co.
Corrigan starred as himself in the 1939 RKO Radio Pictures movie, “The Flying Irishman,” produced by Pandro S. Berman, directed by Leigh Jason, and written by Ernest Pagano and Dalton Trumbo. The movie was released in the United States on 7 April 1939.
On 17 July 1939, Corrigan married Miss Sarah Elizabeth Marvin at San Antonio, Texas. They would have three sons, Douglas, Harry and Roy.
During World War II, Corrigan flew as a test pilot for Douglas Aircraft Company and for the U.S. Army Air Corps Ferrying Command. Later, he became an orange grower. He and his wife lived at a home in the orchards near Santa Ana, California. Mrs. Corrigan died in 1966, and their youngest son, Roy William Corrigan, was killed in an airplane crash on Santa Catalina Island, off the coast of southern California, in 1972.
Clyde Groce (“Douglas”) Corrigan died at St. Joseph’s Hospital, Orange, California, 9 December 1995. He was 88 years old. He was buried at Fairhaven Memorial Park, Santa Ana, California, alongside his wife and son.
¹ On 12 February 1942, The State of Texas Department of Health, Bureau of Vital Statistics, issued a corrected birth certificate, showing Corrigan’s name as “Douglas Corrigan.” The affidavit was sworn to by W.M. Marvin, father of Corrigan’s wife. (NOTE: The original, hand-written certificate of birth gives his name as “Clyde Groce Corrigan.”) His father’s first (given) name was Clyde, and his mother’s middle name was Groce. Corrigan’s younger brother, born the following year, was Harry Groce Corrigan. It seems unlikely that the officially recorded name was in error, as sworn to by Mr. Marvin.
16 July 1983: At 11:10 a.m., a British Airways Sikorsky S-61N-69 Sea King helicopter, c/n 61-770, registration G-BEON, departed Penzance Heliport (PZE) enroute across the Celtic Sea to St. Mary’s Airport, Isles of Scilly. On board were a crew of 3 and 23 passengers. Visibility was poor due to fog. Flying under visual flight rules, the helicopter was at 250 feet (76 meters) while the pilots tried to maintain visual contact with the surface of the calm sea.
Because of the limited visual cues, the crew did not recognize that they were in a slight descent. At approximately 11:35 a.m., the Sikorsky slammed into the ocean at cruise speed. It sank almost immediately. Only six persons survived, including the pilots, Dominic Lawlor and Neil Charleton. The helicopter sank to the sea bed 200 feet (61 meters) below. It was later recovered by the salvage vessel RMAS Seaforth Clansman, along with the bodies of 17 victims.
The official investigation determined that the cause of the accident was pilot error by their failure to recognize and correct the unintentional descent while attempting to fly in conditions not suitable for visual flight. This was the worst helicopter accident in terms of fatalities up to that time.
The Sikorsky S-61N is a civil variant of the United States Navy HSS-2 Sea King. The first S-61N, s/n 61143, first flew 7 August 1962. It is a large twin-engine helicopter with a single main rotor/tail rotor configuration. The S-61N fuselage is 4 feet, 2 inches (1.270 meters) longer than that of the HSS-2. The S-61N is 72 feet, 7 inches (22.123 meters) long and 16 feet, 10 inches (5.131 meters) high, with rotors turning.
The main rotor has five blades and a diameter of 62 feet (18.898 meters). Each blade has a chord of 1 foot, 6.25 inches (0.464 meters). The tail rotor also has five blades and a diameter of 10 feet, 4 inches (3.149 meters). They each have a chord of 7–11/32 inches (0.187 meters). At 100% r.p.m., the main rotor turns 203 r.p.m. and the tail rotor, 1,244 r.p.m. The main rotor turns counter-clockwise, as seen from above. (The advancing blade is on the helicopter’s right side.) The tail rotor turns clockwise, as seen from the left side. (The advancing blade is below.)
G-BEON was powered by two General Electric CT58-140-1 turboshaft engines, each of which had maximum power rating of 1,400 shaft horsepower for takeoff and 1,500 SHP for 2½ minutes. The main transmission was rated for 2,300 horsepower, maximum.
The S-61 has a cruise speed of 166 miles per hour (267 kilometers per hour). The service ceiling is 12,500 feet (3,810 meters). The maximum takeoff weight is 20,500 pounds (9,298.6 kilograms).
Between 1958 and 1980, Sikorsky built 794 S-61 series helicopters. 123 were S-61Ns.