7 July 1965: The McDonnell Aircraft Corporation delivered the 1,000th production F-4 Phantom II, an F-4B, to the United States Navy. Phantom II MSN 1034 was an F-4B-23-MC Phantom II, assigned Bureau of Aeronautics serial number (“Bu. No.”) 152276.
The fighter was assigned to Marine Fighter Attack Squadron 314 (VFMA-314), the “Black Knights,” at Da Nang Air Base, Republic of South Vietnam. On the morning of 24 January 1966, Bu. No. 152276 was flown by Captain Doyle Robert Sprick, USMC, with Radar Intercept Officer 2nd Lieutenant Delmar George Booze, USMC, as one of a flight of four F-4s assigned to drop napalm on a target 7 miles (11 kilometers) southwest of Hue-Phu Bai.
At 10:05 a.m., Captain Albert Pitt, USMC, flying F-4B-22-MC Bu. No. 152265, with RIO 2nd Lieutenant Lawrence Neal Helber, USMC, radioed that he, in company with Captain Sprick, was off the target and returning to Da Nang.
Neither airplane arrived. A search was started at 11:00 a.m. The two-day search was unsuccessful. It is presumed that the two Phantoms collided. All four aviators were listed as missing, presumed killed in action.
7 July 1962: Colonel Georgy Konstantinovich Mosolov, Hero of the Soviet Union, flew the Mikoyan-Gurevich E-152\1 to a two-way average speed of 2,681 kilometers per hour (1,666 miles per hour), setting a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 15/25 Kilometer Straight Course.¹
The E-152\1 (also known as Ye-152-1) was a prototype interceptor, similar to the production MiG-21. In documents submitted to FAI, the E-152\1 was identified as E-166. Colonel Mosolov made the first flight of the E-152\1 on 21 April 1961. The aircraft displayed at The Central Museum of the Air Forces at Monino, Russia, as E-166 is actually the E-152\2, sister ship of Colonel Mosolov’s record-setting prototype.
This airplane set two other FAI world records. Test Pilot Alexander Vasilievich Fedotov flew it to 2,401 kilometers per hour (1,492 miles per hour) over a 100 kilometer course, 10 October 1961² ; and on 11 September 1962, Pyotr Maksimovich Ostapenko set a world record for altitude in horizontal flight of 22,670 meters (74,377 feet feet).³
The Mikoyan Gurevich E-152\1 is a single-place, single-engine delta-winged prototype all-weather interceptor. It is 19.656 meters (64.448 feet) long with a wingspan of 8.793 meters (28.848 feet). The leading edge of the wings are swept back to 53° 47′. The empty weight is 10,900 kilograms (24,030 pounds) and takeoff weight is 14,350 kilograms (31,636 pounds).
It was powered by a Tumansky R-15B-300 turbojet engine producing 22,500 pounds of thrust (100.085 kilonewtons) with afterburner. This was the original engine for the MiG-25.
Maximum speed Mach 2.82 (3,030 kilometers per hour, 1,883 miles per hour) at 15,400 meters (50,525 feet). The service ceiling is 22,680 meters (74,405 feet). Internal fuel capacity is 4,960 liters (1,310 gallons), and the E-152\1 could carry a 1,500 liter (396 gallon) external fuel tank. Its range is 1,470 kilometers (913 miles).
After a two-year test program, E-152\1 and its sistership, E-152\2 were converted to E-152M\1 and E-152M\2.
Georgy Konstantinovich Mosolov was born 3 May 1926 at Ufa, Bashkortostan, Union of Soviet Socialist Republics. He was educated at the Central Aviation Club, where he graduated in 1943, and then went to the Special Air Forces School. In 1945 he completed the Primary Pilot School and was assigned as an instructor at the Chuguev Military Aviation School at Kharkiv, Ukraine.
In 1953 Mosolov was sent to the Ministry of Industrial Aviation Test Pilot School at Ramenskoye Airport, southeast of Moscow, and 6 years later, to the Moscow Aviation Institute. He was a test pilot at the Mikoyan Experimental Design Bureau from 1953 to 1959, when he became the chief test pilot.
Georgy Mosolov set six world speed and altitude records. He was named a Hero of the Soviet Union, 5 October 1960, and Honored Test Pilot of the Soviet Union, 20 September 1967. The Fédération Aéronautique Internationale awarded him its Henry De La Vaulx Medal three times: 1960, 1961 and 1962. The medal is presented to the holder of a recognized absolute world aviation record, set the previous year.
On 11 September 1962, an experimental Mikoyan Ye-8 that Colonel Mosolov was flying suffered a catastrophic compressor failure at Mach 2.15. Engine fragments heavily damaged to prototype and it began to break apart. Severely injured, Mosolov ejected from the doomed airplane at Mach 1.78. He had suffered a severe head injury, two broken arms and a broken leg during the ejection and became entangled in the parachute’s shroud lines. His other leg was broken when he landed in a forest. The following day he suffered cardiac arrest. During a surgical procedure, he went in to cardiac arrest a second time.
Mosolov survived but his test flying career was over. His recovery took more than a year, and though he was able to fly again, he could not resume his duties as a test pilot.
Georgy Mosolov served as an international representative for Aeroflot until 1992. He was also a department head at the Higher Komsomol School (Moscow University for the Humanities).
Mosolov was Chairman of the USSR Hockey Federation from 1969 to 1973. He was an Honored Master of Sports of the USSR.
Colonel Georgy Konstantinovich Mosolov, Soviet Air Forces, Hero of the Soviet Union, died 17 March 2018, at Moscow, Russia, at the age of 91 years. He was buried at the Vagankovsoye cemetery in Moscow.
7 July 1946: At the Hughes Aircraft Company’s private airport in Culver City, California, the first of two prototype XF-11 photographic reconnaissance airplanes took of on its first flight. In the cockpit was Howard Robard Hughes, Jr.
The Hughes XF-11 was designed to be flown by a pilot and a navigator/photographer. Its configuration was similar to the Lockheed P-38 Lightning and Northrop P-61 Black Widow, as well as the earlier Hughes D-2. The prototype was 65 feet, 5 inches (19.939 meters) long with a wingspan of 101 feet, 4 inches (30.886 meters) and height of 23 feet, 2 inches (7.061 meters). The empty weight was 37,100 pounds (16,828.3 kilograms) and maximum takeoff weight was 58,300 pounds (26,444.4 kilograms).
The XF-11 was powered by two air-cooled, supercharged 4,362.49-cubic-inch-displacement (71.49 liter) air-cooled, supercharged Pratt & Whitney R-4360-31 (Wasp Major TSB1-GD) four row, 28-cylinder radial engines. This engine had a compression ratio of 7:1. It had a normal power rating of 2,550 horsepower at 2,550 r.p.m. at 5,000 feet (1,524 meters), and 3,000 horsepower at 2,700 r.p.m. for takeoff. The R-4360-31 was 4 feet, 4.50 inches (1.334 meters) in diameter, 9 feet, 6.25 inches (2.902 meters) long and weighed 3,506 pounds (1,590 kilograms). The engines drove a pair of counter-rotating four-bladed propellers through a 0.381:1 gear reduction.
The planned maximum speed was 450 miles per hour (724 kilometers per hour), service ceiling 44,000 feet (13,411 meters) and planned range was 5,000 miles (8,047 kilometers).
After about an hour of flight, a hydraulic fluid leak caused the rear propeller of the right engine to go into reverse pitch. Rather than shutting the engine down and feathering the propellers to reduce aerodynamic drag, Hughes maintained full power on the right engine but reduced power on the left, attempting to limit adverse yaw to the right side.
Unable to make it back to the Culver City airport, Hughes planned to land at the Los Angeles Country Club. At 7:20 p.m., the airplane crashed into three houses on North Whittier Drive, Beverly Hills, California. The fire destroyed the prototype and one of the houses and heavily damaged the others. Howard Hughes was seriously injured in the crash.
The investigating board criticized Hughes for not following the flight test plan, staying airborne too long, and deviating from a number of standard test flight protocols. The cause of the actual crash was determined to be pilot error.
A second XF-11 was completed and flew in April 1947, again with Hughes in the cockpit. The project was cancelled however, in favor of the Northrop F-15 Reporter and Boeing RB-50 Superfortress, which were reconnaissance aircraft based on existing combat models already in production.
6 July 1944: In honor of Her Royal Highness The Princess Elizabeth, a United States Army Air Forces heavy bomber, Boeing B-17G-55-BO Flying Fortress 42-102547, was christened Rose of York. The ceremony took place at R.A.F. Thurleigh (U.S.A.A.F. Station 111), 5 miles (8 kilometers) north of Bedford, Bedfordshire, England.
Named for Princess Elizabeth Windsor (now, Her Majesty, Queen Elizabeth II), 42-102547 was originally named Princess Elizabeth but that did not meet with any official approval. (There were concerns about the propaganda value to the enemy, and the effect on civilian morale, should the bomber named for a member of the Royal Family be lost in combat.) The aircraft was renamed Rose of York instead and was christened by the Princess on her royal visit to the airfield.
Following the ceremony, the bomber was flown to RAF Molesworth, where a number of photographs were taken.
42-102547 was built by the Boeing Airplane Company at its Plant 2, south of Seattle, Washington, in early 1944. The new bomber was not camouflaged, but left in its natural metal finish. It was flown to the Cheyenne Modification Center, Cheyenne, Wyoming, on 12 March 1944, for installation of the latest combat modifications. It was then taken to the B-17 training base at Grand Island Army Air Field in central Nebraska. From there, it flew to Dow Army Air Field, Bangor Maine, arriving 3 April 1944, and then ferried across the North Atlantic Ocean to England.
The Flying Fortress arrived in England, and on 2 May 1944, was assigned to the 401st Bombardment Group, Heavy, at R.A.F. Deenethorpe (A.A.F. Station 128). Three days later, though, 42-102547 was transferred to the 306th Bombardment Group, Heavy, at R.A.F. Thurleigh. It was assigned to Captain Perry E. Raster of the 367th Bombardment Squadron, Heavy. The group’s identification code, “Triangle H”—a white capital “H” centered on a black triangle—was painted on the vertical fin above the serial number. A black capital “F” was painted below, identifying the individual airplane within its squadron.
42-102547 had completed 13 combat missions by 6 July 1944.
On Saturday, 3 February 1945, the Eighth Air Force, under the command of Lieutenant General James Harold (“Jimmy”) Doolittle, executed Mission No. 817. 1,003 B-17 Flying Fortresses, 434 B-24 Liberators and 948 P-47 and P-51 fighters were sent to attack Berlin, the capital of the Third Reich. The B-17s’ primary target was the city’s railroad marshaling yards, while the B-24s attacked the Braunkohle Benzine A.G. synthetic oil refinery at Rothensee.
23 B-17s, 2 B-24s, 7 P-51s and 1 P-47 were lost. 6 B-17s and 2 P-51s were damaged beyond repair, and another 339 B-17s and 58 B-24s were damaged.
18 airmen were killed in action, with 11 wounded and 216 missing.
Rose of York was one of the B-17s on that 1,000-bomber mission to Berlin. On its sixty-third combat mission, and with a different crew, 42-102547 was hit by heavy and accurate anti-aircraft fire. The last contact indicated that one engine was out of operation and another was streaming gasoline. The Flying Fortress went down in the English Channel with all nine crew members and a civilian news reporter.¹
The B-17G was the final production variant of the Flying Fortress. It entered service with the United States Army Air Forces in 1943.
The Boeing B-17G Flying Fortress was a four-engine heavy bomber operated by a combat crew of nine to ten men. It was 74 feet, 8.90 inches (22.781 meters) long with a wingspan of 103 feet, 9.38 inches (31.633 meters) and an overall height of 19 feet, 1.00 inch (5.187 meters). The wings have 3½° angle of incidence and 4½° dihedral. The leading edges are swept aft 8¾°. The total wing area is 1,426 square feet (132.48 square meters). The horizontal stabilizer has a span of 43 feet (13.106 meters) with 0° incidence and dihedral. Its total area, including elevators, is 331.1 square feet (12.18 square meters). The B-17G had an empty weight of 35,972 pounds (16,316.6 kilograms), and the maximum takeoff weight was 67,860 pounds (30,780.8 kilograms).
The B-17G was powered by four air-cooled, supercharged, 1,823.129-cubic-inch-displacement (29.876 liters) Wright Cyclone C9GC (R-1820-97) nine-cylinder radial engines with a compression ratio of 6.70:1. The engines were equipped with remote General Electric turbochargers capable of 24,000 r.p.m. The R-1820-97 had a Normal Power rating of 1,000 horsepower at 2,300 r.p.m. at 25,000 feet (7,620 meters), and 1,200 horsepower at 2,500 r.p.m. for Takeoff and Military Power. The engine could produce 1,380 horsepower at 2,500 r.p.m., War Emergency Power. 100-octane aviation gasoline was required. The Cyclones turned three-bladed, constant-speed, Hamilton Standard Hydromatic propellers with a diameter of 11 feet, 7 inches (3.835 meters) through a 0.5625:1 gear reduction. The R-1820-97 engine was 3 feet, 11.80 inches (1.214 meters) long and 4 feet, 7.10 inches (1.400 meters) in diameter, and weighed 1,315 pounds (596 kilograms).
The B-17G had a cruising speed of 172 knots (198 miles per hour/319 kilometers per hour) at 10,000 feet (3,048 meters). The maximum speed was 285 knots (328 miles per hour/528 kilometers per hour) at 26,700 feet (8,138 meters). The service ceiling was 38,450 feet (11,720 meters) at maximum power.
The B-17G had a fuel capacity of 2,780 gallons (10,523 liters) in twelve wing tanks. Two “Tokyo tanks” could be installed in the bomb bay, increasing capacity by 820 gallons (3,104 liters). The B-17G combat radius of 689 nautical miles (793 statute miles/1,276 kilometers) with max bomb load, and a maximum ferry range of 2,624 nautical miles (3,031 statute miles/4,878 kilometers).
The B-17G was armed with thirteen Browning AN-M2 .50-caliber machine guns for defense against enemy fighters. Power turrets mounting two guns each were located at the nose, dorsal, and ventral positions. Two guns could be installed in flexible mounts in the nose compartment, one in the radio compartment, two in the waist and two in the tail. 5,970 rounds of ammunition were carried.
The maximum bomb load of the B-17G was 12,800 pounds (5,806 kilograms). The internal bomb bay could be loaded with a maximum of ten 1,000 pound bombs, eight 1,600 pound (725.75 kilogram) bombs or two 2,000 pound bombs. The physical size of each type limited the number that could be carried in the bomb bay.
The B-17 Flying Fortress was in production from 1936 to 1945. 12,731 B-17s were built by Boeing, Douglas Aircraft Company and Lockheed-Vega. (The manufacturer codes -BO, -DL and -VE follows the Block Number in each airplane’s type designation.) 8,680 of these were B-17Gs, with 4,035 built by Boeing, 2,395 by Douglas and 2,250 by Lockheed-Vega.
¹ Missing Air Crew Report (MACR) 12283: Aircraft Commander, Lieutenant Vernon Daley; Co-pilot: 2nd Lieutenant Joseph Carbine; Navigator, 1st Lieutenant Paul Becker; Bombardier/Nose Gunner, Staff Sergeant Robert Crede; Flight Engineer/Top Turret Gunner, Technical Sergeant Reisel Horn; Radio Operator/Top Gunner, Technical Sergeant Porfirio Marquez; Ball Turret Gunner: Staff Sergeant George Petrillo; Waist gunner, Staff Sergeant Silvio DeZolt; Tail Gunner: Sergeant Okey Coplin; and British Broadcasting Company (BBC) war corresponent Guy Byam (civilian). 10 Killed in Action.
6 July 1939: Ольга Васильевна Клепикова(Olga Vasil’yevna Klepikova) flew an Antonov RF-7 glider from Tushino airport, Moscow, to Mikhaylovka, in the Stalingrad region of the Russian Soviet Federative Socialist Republic. She set two Fédération Aéronautique Internationale (FAI) World Records for Distance at 749.203 kilometers (465.533 statute miles).¹
Klepikova’s glider was towed aloft by a Polikarpov P-5 biplane, and then released at an altitude of 1,000 meters (3,281 feet). She circled overhead for approximately an hour, gaining altitude, before heading toward Stalingrad. The total duration of the flight was 8 hours, 25 minutes.
Once she landed near Mikhaylovka, Tovarisch (Comrade) Klepikova was captured by “vigilant farmers” who presumed that she was a German spy. They turned her over to the NKVD (Narodnyy Komissariat Vnutrennikh Del), the infamous predecessor to the KGB.
Olga Vasil’yevna Klepikova was born at Tula, about 120 miles (193 kilometers) south of Moscow, on 10 October 1915.
Gospohzha Klepikova studied at the Tula FZU (Fabrichno-Zavodskoe Uchilishe), an industrial technical school, and she then worked as a lathe operator in an armaments factory.
Comrade Klepikova joined the Tula Aero Club in 1930, where she was taught to fly. In 1933, she was sent to Moscow as an instructor for the Central Aero Club at Tushino.
During the Great Patriotic War, Comrade Klepikova served as a flight instructor at Stalingrad. She worked as a test pilot at Kazan and then Rostov on Don from the end of the War until 1953.
Gospohzha Klepikova married a fellow test pilot, and they had two daughters. The family relocated to the area of Kiev, Ukraine. As of 2002, she lived in Vasiljena, Kiev, Ukraine, with a pension equivalent to $20 per month.
Olga Vasil’yevna Klepikova, an Honored Master of Sports of the USSR, died at Kiev, 27 July 2010, at the age of 95 years. Her remains were interred at the Baikove Cemetery in Kiev.
Gospohzha Klepikova’s glider was a Рот-Фронт-7 (Rot-, or Roth-Front 7), designed by Oleg Konstantinovich Antonov. It was one of five built at the Moscow Glider Factory. The Rot-Front 7 was a single-place, high wing monoplane glider, constructed primarily of wood. It was covered with 1.5–3.5 millimeter thick plywood. Wing flaps allowed the glider to land in fairly small areas. The RF-7 was 5.00 meters (16 feet, 4.9 inches) long, with a wingspan of 16.24 meters (53 feet, 3.4 inches), and height of 1.55 meters (5 feet, 1.0 inches). The wings had a total area of 12.5 square meters (134.6 square feet), with an aspect ratio of 22.5. As much as 120 liters (31.7 gallons) of water ballast was carried in a tank behind the pilot. There was a single, retractable wheel under the ballast tank, which was enclosed by two aluminum doors.
The RF-7 had a best cruise speed of 85 kilometers per hour (52.8 miles per hour), and it had a maximum speed of 88 kilometers per hour (54.6 miles per hour).
The Rot-Front 7 was considered to be the best aerobatic glider of its time, and was designed to withstand a load factor of 8 gs.
¹ FAI Record File Number 4386: World Record for Distance, Class D, Feminine: 749.20 kilometers (465.53 statute miles); and FAI Record File Number 13606: World Record for Distance, Class D, General: 749.203 kilometers (465.533 statute miles).