20 June 1941: The Department of War established the United States Army Air Forces. The new organization consisted of Headquarters Army Air Forces, the newly-formed Air Force Combat Command, and the existing United States Army Air Corps. The U.S.A.A.F. was placed under the command of Major General Henry Harley (“Hap”) Arnold, Chief of the Air Forces.
At the end of 1941, the U.S. Army Air Forces had a strength of 354,161 (24,521 officers and 329,640 enlisted) and 12,297 aircraft, with 4,477 of these classified as combat aircraft. Over the next 3 years, personnel would increase to a peak of 2,411,294. The number of aircraft reached a maximum 79,908 by July 1944.
The most advanced aircraft in the inventory of the Army Air Forces at its inception were the Boeing B-17C/D Flying Fortress heavy bomber, the North American B-25 Mitchell and Martin B-26 Marauder medium bombers, Lockheed P-38D Lighting, Bell P-39D Airacobra and Curtiss Wright P-40B Warhawk fighters, and the Douglas C-39 transport. Many older designs remained in service.
On 18 September 1947, the United States Army Air Forces was detached from the United States Army and became a separate military service, the United States Air Force.
On 21 December 1944, General Arnold was promoted to a five-star rank, General of the Army. On 7 May 1949, his rank was officially changed to General of the Air Force.
18–20 June 1937: The number 1 prototype Tupolev ANT-25, with pilot Valery Pavlovich Chkalov, Georgy Filippovich Baydukov (co-pilot/radio/navigator) and Alexander Vasilyevich Belyakov (radio/navigator) departed Shchelkovo airfield near Moscow, Russia, at 4:04 a.m. (01:04 GMT), 18 June, and flew north along the E. 38° meridian toward the North Pole, and beyond that, south along the W. 123°meridian toward San Francisco, California, U.S.A.
The Tupolev ANT-25RD was an experimental very longrange airplane, built by OJSC Voronezh, intended to set distance records. It also served as a prototype for a long-range bomber, which was designated DB-1.
The ANT-25 was a single-engine low-wing monoplane, primarily of metal construction, with retractable landing gear. The wings and horizontal stabilizer were covered with corrugated sheet metal. The troughs were filled with balsa wood to create a smoother surface. It was flown by a crew of three. The pilot was placed directly behind the engine, followed by a crew rest area, then the navigator/radio operator’s station. The copilot flew the airplane from a small enclosed cockpit behind the navigator’s station.
The airplane was 13.00 meters (42 feet, 8 inches) long with a wingspan of 34.00 meters (111 feet, 7 inches) long and overall height of 5.5 meters (18 feet, ½-inch). The very high aspect ratio wing (13:1) has an area of 87.10 square meters (937.54 square feet), because of its length, the wing used steel spars. The ANT-25 had an empty weight of 3,784 kilograms (8,342 pounds) and maximum gross weight of 10,000 kilograms (22,046 pounds).
The ANT-25 was powered by a single liquid-cooled, supercharged, 46.928 liter (2,863.722 cubic inches) Mikulin M-34RD single overhead cam 60° V-12 engine, rated at 830 horsepower. Right and left cylinder banks had different length connecting rods: 190mm vs. 199mm. Drove a three-blade propeller with a diameter of 3.9 meters (12.8 feet) through gear reduction. The pitch of the propeller blades could be adjusted prior to flight.
The ANT-25 cruise speed 165 km/h (103 miles per hour), max, 244 km/h (152 miles per hour), range 10,800 km (6,711 miles) Ceiling 7,850m (25,755 feet)
Tupolev ANT-25 URSS N025
Moscow to Pearson Airfield, Vancouver, Washington
9,130 kilometers ( miles) 63 hours, 16 minutes
4:05 a.m., Moscow (01:05 GMT) Shchelkovo airfield 38°E. > North Pole>123°W San Francisco
encountered storm/propeller icing/climb 3,000m
19 June 04:15, researchers at North Pole 1 heard the airplane
over Canadian arctic climbed to 5,750m to clear clouds temps 0° C., O2 limited
19 June 13:50 Canadian coast/turned west/Rocky Mountains/6,100m -20° C.
20 June 00:40 out of O2
Fly along Pacific coast
Vancouver 20 June 16:20 GT
Headwinds used more fuel; URSS national record
Pres FDR spoke w/ crew for 1+40
Airplane disassembled and shipped back to Soviet Union
20 June 1937: Leg 22. Amelia Earhart and Fred Noonan fly the Electra from Rangoon to Bangkok then on to Singapore.
“Moist clouds were our companions as we left Rangoon the next morning, bound for Bangkok, Siam. First, we crossed the upper reaches of the Gulf of Martaban, flying over Moulmein. . . A great range of mountains extends north and south along the western border of Siam, separating it from the long arm of Burma that reaches down into the Malay Peninsula. Through squally weather we climbed to 8,000 feet and more, topping this mountain barrier. On its eastern flanks the clouds broke and there stretched before us a dark green forest splashed with patches of bright color, cheerful even in the eyes of a pilot who recognized in all the limitless view no landing place. The country fell away gradually to the east, the hills flattening out into heavy jungle. Then we crossed the Mei Khlaung River, with little villages scattered along its banks, the wide expanses of irrigated land burdened with rice crops.
“Bangkok itself lies in a vast plain with mountains in the distant background. . . After refueling at Bangkok (the airport was one of the best we encountered) we started for Singapore, more than 900 miles away. . . Though we did not sight them, there were two transport planes that day on the same route which we flew. The Imperial Airways machine left Rangoon first and the K.L.M. Douglas at daybreak. Our Wasp-motored Lockheed left fifteen minutes later. All stopped at Bangkok, then followed different courses to Singapore. We arrived there first, at 5:25 P.M. local time, because we cut straight and did not stop along the way.” —Amelia Earhart
Amelia Earhart wrote beautifully. Her notes are full of color and texture. She describes the land and the sea and the sky, the towns and cities and the people. Her descriptions bring all of these to life.
For conspicuous gallantry and intrepidity at the risk of his life above and beyond the call of duty on 19 June 1968 as pilot and aircraft commander of a search and rescue helicopter, attached to Helicopter Support Squadron Seven, Detachment One Hundred Four, embarked in USS Preble (DLG 15), during operations against enemy forces in North Vietnam.
Launched shortly after midnight to attempt the rescue of two downed aviators, Lieutenant (then Lieutenant, Junior Grade) Lassen skillfully piloted his aircraft over unknown and hostile terrain to a steep, tree-covered hill on which the survivors had been located.
Although enemy fire was being directed at the helicopter, he initially landed in a clear area near the base of the hill, but, due to the dense undergrowth, the survivors could not reach the helicopter. With the aid of flare illumination, Lieutenant Lassen successfully accomplished a hover between two trees at the survivor’s position. Illumination was abruptly lost as the last of the flares were expended, and the helicopter collided with a tree, commencing a sharp descent.
Expertly righting his aircraft and maneuvering clear, Lieutenant Lassen remained in the area, determined to make another rescue attempt, and encouraged the downed aviators while awaiting resumption of flare illumination. After another unsuccessful, illuminated, rescue attempt, and with his fuel dangerously low and his aircraft significantly damaged, he launched again and commenced another approach in the face of the continuing enemy opposition.
When flare illumination was again lost, Lieutenant Lassen, fully aware of the dangers in clearly revealing his position to the enemy, turned on his landing lights and completed the landing. On this attempt, the survivors were able to make their way to the helicopter. Enroute to the coast, Lieutenant Lassen encountered and successfully evaded additional hostile antiaircraft fire and, with fuel for only five minutes of flight remaining, landed safely aboard USS Jouett (DLG 29).
His courageous and daring actions, determination, and extraordinary airmanship in the face of great risk sustain and enhance the finest traditions of the United States Naval Service.
Lieutenant (Junior Grade) Clyde Everett Lassen was the Officer in Charge of Detachment 104 of Helicopter Support Squadron SEVEN (HC-7), the “Sea Devils,” aboard USS Preble (DLG-15). The assignment was Combat Search and Rescue.
On the night of 18/19 June 1968, a flight of three aircraft from the aircraft carrier USS America (CV-66) were on a bombing mission over North Vietnam. Root Beer 210 was a McDonnell Douglas F-4J-33-MC Phantom II, Bu. No. 155546, flown by Lieutenant Commander John “Claw” Holtzclaw and Lieutenant Commander John A. “Zeke” Burns. Shortly after midnight, two SA-2 surface to air missiles were fired at the Phantom. Holtzclaw and Burns evaded them, but a third missile detonated very close to the fighter bomber, destroying the outer one-third of the right wing. With their airplane critically damaged and on fire, the two naval aviators were forced to eject over enemy territory. They parachuted into a rice paddy and could hear enemy soldiers talking nearby. Burns had suffered a broken leg as well as other injuries.
Aboard the guided missile frigate USS Preble (DLG-15), Lieutenant (junior grade) Clyde Lassen and his flight crew were awakened and assigned to rescue the crew of Root Beer 210, 70 miles (113 kilometers) away in total darkness. Lassen and his co-pilot, Lieutenant (j.g.) LeRoy Cook and gunners Aviation Electrician’s Mate 2nd Class (AE2) Bruce Dallas and Aviation Machinist’s Mate 3rd Class (ADJ3) Don West, took off from Preble at 0022 hours aboard their Kaman SH-2A Seasprite helicopter, call sign Clementine Two, and were vectored by radar to the location of the downed aircrew. The glow of the burning Phantom could be seen from 30 miles (48 kilometers) away. They arrived on scene at 0141 hours. Holtzclaw and Burns were in immediate need of rescue as the enemy was closing in.
Holtzclaw and Burns were on a hillside covered with very tall trees, making it impossible for the Seasprite to land. Parachute flares dropped by supporting aircraft illuminated the area. The pickup would have to be made using a “jungle penetrator” attached to the helicopter’s rescue hoist. But the single-engine helicopter was already fully loaded with its four-man crew and their weapons and ammunition. It could not pick up both fliers while hovering out of ground effect above the trees. Lassen ordered his co-pilot to dump fuel to reduce the weight.
As Lassen hovered into position to make the hoist pickup, the overhead flares went out, leaving the jungle totally dark. Unable to see, Lassen collided with a tree causing damage to the horizontal stabilizer and the right side cabin door. He narrowly avoided a crash.
Clementine Two moved away while they awaited the arrival of another flare aircraft. They were soon engaged by enemy ground fire and the helicopter gunners returned fire with their M-60 machine guns.
On several occasions, Lassen landed the SH-2A in a rice paddy to pickup Holtzclaw and Burns, but enemy gunfire prevent them from reaching the helicopter, which repeatedly had to pull back.
Finally, the crew of Root Beer 210 found their way to the bottom of the slope and Clementine Two landed in a rice paddy about 60 yards (55 meters) away. A fierce firefight between the North Vietnamese soldiers and the gunners of the Navy helicopter took place. Lassen held the Seasprite in a hover to prevent it from sinking into the mud. The gunners jumped down to assist Holtzclaw and Burns aboard. As soon as they were loaded, Lassen immediately took off and left the area, climbed to 4,000 feet (1,220 meters) and headed toward the South China Sea, twenty miles (32 kilometers) away. The helicopter had only thirty minutes of fuel remaining. During the flight, the right cabin door, which had been damaged when the helicopter hit the tree, came off and fell away into the darkness.
Clementine Two was too far away to make it back to Preble, so they turned toward USS Jouett (DLG-29). Commander Destroyer Squadron One, Captain Robert Hayes, commanding Jouett, turned his ship toward the shore and proceeded at full speed, turning on all of the ship’s lights so that Lassen would be able to find it. Jouett came within 3 miles (4.8 kilometers) of the beach. With almost no fuel remaining, Lassen made a straight-in approach and landing.
For his actions on 19 June 1968, Lieutenant Clyde Everett Lassen was awarded the Medal of Honor. Lieutenant (j.g.) LeRoy Cook received the Navy Cross. AE2 Bruce Dallas and AE3 Don West each received the Silver Star.
Clementine Two was a Kaman SH-2A Seasprite, Bu. No. 149764 (c/n 66). The SH-2A is 52 feet, 2.2 inches (15.905 meters) long with rotors turning, with an overall height of 14 feet, 8.6 inches (4.486 meters). The four-bladed main rotor has a diameter of 44 feet, 0 inches (13.411 meters) and rotates counter-clockwise, as seen from above (the advanicng blade is on the helicopter’s right). The blades are controlled by Kaman’s unique servo flap system. The three-bladed tail rotor is mounted on the left side of a pylon and rotates clockwise, as seen from the helicopter’s left (The advancing blade is below the axis of rotation). The helicopter’s main landing gear was retractable. The SH-2A has and empty weight is 6,110 pounds (2,771 kilograms) and maximum takeoff weight is 10,000 pounds (4,536 kilograms).
The SH-2A is powered by a single General Electric T58-GE-8B turbine engine. The T58 is a free power turboshaft, with a 10-stage axial-flow compressor section, an annular combustion chamber with 16 burner nozzles, and a 3-stage turbine (2 gas-generator stages and a single power-turbine stage). The T58-GE-8B has a Normal Power rating of 1,050 shaft horsepower at 19,500 r.p.m. at Sea Level, and Military Power rating of 1,250 shaft horsepower at 19,500 r.p.m. The engine is 1 foot, 8.9 inches (0.531 meters) in diameter, 4 feet, 11.0 inches (1.499 meters) long, and weighs 305 pounds (138 kilograms).
The SH-2A Seasprite has a Hover Ceiling Out of Ground Effect (HOGE) of 4,600 feet (1,402 meters). With a crew of four, the hover ceiling is reduced to 2,800 feet (853 meters). Its service ceiling is 15,000 feet (4,572 meters).
The SH-2A has a cruise speed of 125 knots (144 miles per hour/232 kilometers per hour) and a maximum speed of 140 knots (161 miles per hour/259 kilometers per hour) at Sea Level. Its combat radius is 125 nautical miles (144 miles/232 kilometers). The maximum range is 465 nautical miles (535 miles/861 kilometers).
Clementine 2 was armed with two M60 7.62 mm machine guns.
88 UH-2As were built 1959-1960, before production shifted to a twin-engine variant.
Seasprite 149764 was lost in the South China Sea, 7 January 1969.
Clyde Everett Lassen was born at Fort Myers, Florida, 14 March 1942. He graduated from Venice High School, Englewood, Florida, in 1960.
Lassen enlisted in the United States Navy, 14 September 1961. He served as an Aviation Electronics Technician, 3rd Class (AT3). In 1964, he was accepted as a Naval Aviation Cadet at NAS Pensacola. On completion of flight training, Lassen was commissioned an ensign and awarded the wings of a Naval Aviator.
Ensign Lassen married Miss Linda Barbara Sawn in October 1965.
He was promoted to lieutenant (junior grade), 16 December 1966, and to lieutenant, 1 July 1968.
President Lyndon Johnson presented the Medal of Honor to Lieutenant Lassen at a ceremony at The White House, 16 January 1969.
Lieutenant Lassen was promoted to the rank of lieutenant commander 1 August 1972, and to commander, 1 July 1975. Commander Lassen retired from the U.S. Navy in December 1982.
Commander Lassen donated his Medal of Honor to the National Naval Aviation Museum 19 June 1993.
Commander Clyde Everett Lassen, United States Navy, died 1 April 1994 at Pensacola, Florida. He was buried at the Barrancas National Cemetery at Pensacola.
Highly recommended: “Clementine Two: U.S. Navy night rescue over North Viet Nam,” by C. LeRoy Cook, athttp://www.vhpa.org/stories/clem2.pdf
19 June 1947: At Muroc Army Airfield (now, Edwards Air Force Base) Colonel Albert Boyd, United States Army Air Forces, set a Fédération Aéronautique Internationale (FAI) World Record for Speed Over a 3 Kilometer Course, with an average speed of 1,003.81 kilometers per hour (623.74 miles per hour).¹ This was not just a class record, but an absolute world speed record.
Col. Boyd flew the Lockheed P-80R Shooting Star, serial number 44-85200, four times over the course, twice in each direction. The record speed was the average of the two fastest consecutive runs. As can be seen in the above photograph, these runs were flown at an altitude of approximately 70 feet (21 meters).
Originally a production P-80A-1-LO Shooting Star, 44-85200 had been converted to the XP-80B, a single prototype for the improved P-80B fighter.
The P-80A-1-LO was a single-place, single-engine, low-wing monoplane powered by a turbojet engine. It was a day fighter, 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, 10½ inches (11.849 meters) and overall height of 11 feet, 4 inches (3.454 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 P-80A-1 was powered by an Allison J33-A-9 or -11 turbojet, rated at 3,850 pounds of thrust (17.126 kilonewtons). It had a maximum speed of 558 miles per hour (898 kilometers per hour) at Sea Level and a service ceiling of 45,000 feet (13,716 meters).
The P-80A was armed with six Browning .50-caliber machine guns grouped together in the nose.
After modification to the XP-80B configuration, 44-85200 was powered by an Allison J33-A-17 with water/alcohol injection. It was rated at 4,000 pounds of thrust (17.793 kilonewtons). Fuel capacity was reduced by 45 gallons (170 liters) to allow for the water/alcohol tank. This was also the first American-built fighter to be equipped with an ejection seat.
The P-80B was heavier than the P-80A, with an empty weight of 8,176 pounds (3,709 kilograms) and gross weight of 12,200 pounds (5,534 kilograms). Visually, the two variants are almost identical.
The XP-80B had a maximum speed of 577 miles per hour (929 kilometers) per hour at 6,000 feet (1,829 meters), a 19 mile per hour (31 kilometers per hour) increase. The service ceiling increased to 45,500 feet (13,868 meters).
44-85200 was next modified to the XP-80R high-speed configuration. The canopy was smaller, the wings were shortened and their leading edges were re-contoured. In its initial configuration, the XP-80R retained the J33-A-17 engine, and incorporated new intakes designed by the National Advisory Committee for Aeronautics (NACA).
The initial performance of the XP-80R was disappointing. The intakes were returned to the standard shape and the J33-A-17 was replaced by a J33-A-35 engine. This improved J33 would be the first turbojet engine to be certified for commercial transport use (Allison Model 400). It was rated at 5,200 pounds of thrust (23.131 kilonewtons) at 11,750 r.p.m. at Sea Level, and 5,400 pounds of thrust (24.020 kilonewtons) with water/methanol injection.
The J33 was a single-spool turbojet with a single-stage centrifugal-flow compressor, 14 combustion chambers, and a single-stage axial-flow turbine. The J33-A-35 had a maximum diameter of 4 feet, 1.2 inches (1.250 meters) and was 8 feet, 8.5 inches (2.654 meters) long. It weighed 1,795 pounds (814 kilograms).
Technicians who modified the XP-80R at Lockheed Plant B-9 Production Flight Test Center, Metropolitan Airport, Van Nuys (just a few miles west of the main plant in Burbank). nicknamed the modified Shooting Star “Racey.”
Lockheed XP-80R 44-85200 is in the collection of the National Museum of the United States Air Force at Wright-Patterson Air Force Base, Ohio.
At the time of the speed record flight, Colonel Boyd was chief of the Flight Test Divison at Wright Field, Dayton, Ohio.
Albert Boyd was born 22 November 1906 at Rankin, Tennessee, the first of three sons of Kester S. Boyd a school night watchman, and Mary Eliza Beaver Boyd. In 1924, Boyd graduated from high school in Asheville, North Carolina, then attended Buncombe Junior College in Asheville.
Boyd was one of the most influential officers to have served in the United States Air Force. He entered the U.S. Army Air Corps as an aviation cadet 27 October 1927. After completion of flight training at Maxwell Field, Alabama, Boyd was commissioned as a second lieutenant, Air Corps Reserve, 28 February 1929, and as a second lieutenant, Air Corps, 2 May 1929.
Lieutenant Boyd married Miss Anna Lu Oheim at San Antonio, Texas, 8 September 1933. She was the daughter of Mr. and Mrs. G.F. Oheim of New Braunfels, Texas, (1907–1981).
He was promoted to 1st lieutenant 1 October 1934. On 24 July 1936, Boyd was promoted to the temporary rank of captain. This rank became permanent 2 May 1939. For the next five years, Lieutenant Boyd served as a flight instructor at Maxwell Field, Alabama, an then Brooks, Kelly and Randolph Fields in Texas.
In 1934, 1st Lieutenant Boyd was assigned as engineering and operations officer at Chanute Field, Rantoul, Illinois. He completed the Air Corps technical School and the Engineer Armament Course. On 24 July 1936, Boyd was promoted to the temporary rank of captain. This rank became permanent 2 May 1939. In 1939 he was assigned to the Hawaiian Air Depot as assistant engineering officer, and was promoted to major (temporary), 15 March 1941. He and Mrs. Boyd lived in Honolulu. His Army salary was $3,375 per year. In December 1941, he became the chief engineering officer.
On 5 January 1942, Major Boyd was promoted to lieutenant colonel (temporary) and rated a command pilot. Following the end of World War II, Boyd reverted to his permanent rank of major, 2 May 1946.
In October 1945, Major Boyd was appointed acting chief of the Flight Test Division at Wright Field. He became chief of the division, October 1945, and also flew as an experimental test pilot. Boyd believed that it was not enough for Air Force test pilots to be superior pilots. They needed to be trained engineers and scientists in order to properly evaluate new aircraft. He developed the Air Force Test Pilot School and recommended that flight testing operations be centered at Muroc Field in the high desert of southern California, where vast open spaces and excellent flying conditions were available. He was the first commander of the Air Force Flight Test Center.
When Brigadier General Boyd took command of Muroc Air Force Base in September 1949, he recommended that its name be changed to honor the late test pilot, Glen Edwards, who had been killed while testing a Northrop YB-49 near there, 5 June 1948. Since that time the airfield has been known as Edwards Air Force Base.
In February 1952, General Boyd was assigned as vice commander of the Wright Air Development Center, and commander, June 1952. His final assignment on active duty was as deputy commander of the Air Research and Development Command at Baltimore, Maryland, from 1 August 1955.
From 1947 until he retired in 1957 as a major general, Albert Boyd flew and approved every aircraft in use by the U.S. Air Force. By the time he retired, he had logged over 21,120 flight hours in more than 700 different aircraft. He had been awarded the Legion of Merit, the Distinguished Flying Cross and the Distinguished Service Medal.
Major General Albert Boyd retired from the Air Force 30 October 1957 following 30 years of service. During his military career, he had been awarded the legion of Merit and the Distinguished Flying Cross. General Boyd died at Saint Augustine, Florida, 18 September 1976 at the age of 69 years. He is buried at the Arlington National Cemetery.