Curtiss-Wright’s Chief Test Pilot, H. Lloyd Child, in the cockpit of a P-40 Warhawk, circa 1940. (Rudy Arnold Collection/NASM)
26 April 1939: The United States Army Air Corps placed an order for 524 Curtiss-Wright P-40 Warhawks. This was the largest production order for any U.S.-built fighter since World War I. The total cost was $12,872,398.¹
The order was authorized by the Air Corps Expansion Act, approved by Congress 3 April, and signed by President Roosevelt on 26 April 1939.
The Curtiss-Wright Corporation Hawk 81 (P-40 Warhawk) was a single-seat, single-engine pursuit, designed by Chief Engineer Donovan Reese Berlin. It was developed from Berlin’s radial-engine P-36 Hawk. The P-40 was a low-wing monoplane of all-metal construction and used flush riveting to reduce aerodynamic drag. It had an enclosed cockpit and retractable landing gear (including the tail wheel). Extensive wind tunnel testing at the NACA Langley laboratories refined the airplane’s design, significantly increasing the top speed.
The first production Curtiss-Wright P-40 Warhawk, 39-156. (U.S. Air Force)
The new fighter was 31 feet, 8-9/16 inches (9.666 meters) long with a wingspan of 37 feet, 3½ inches (11.366 meters) and overall height of 9 feet, 7 inches (2.921 meters). The P-40’s empty weight was 5,376 pounds (2,438.5 kilograms) and gross weight was 6,787 pounds (3,078.5 kilograms).
The P-40 was powered by a liquid-cooled, supercharged, 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Co. V-1710-C15 (V-1710-33). This was a single overhead cam (SOHC) 60° V-12 engine designed by Harold Caminez, Allison’s chief engineer. The V-1710-33 had a compression ratio of 6.65:1. It was rated at 930 horsepower at 2,600 r.p.m. at 12,800 feet (3,901 meters), and 1,040 horsepower at 2,800 r.p.m. for takeoff, burning 100-octane gasoline. The engine turned a three-bladed Curtiss Electric constant-speed propeller through a 2:1 gear reduction. The V-1710-33 was 8 feet, 2.54 inches (2.503 meters) long, 3 feet, 5.88 inches (1.064 meters) high, and 2 feet, 5.29 inches (0.744 meters) wide. It weighed 1,340 pounds (607.8 kilograms).
Allison Engineering Co. V-1710-33 V-12 aircraft engine at the Smithsonian Institution National Air and Space Museum Steven F. Udvar-Hazy Center. (NASM)
The cruising speed of the P-40 was 272 miles per hour (438 kilometers per hour) and the maximum speed was 357 miles per hour (575 kilometers per hour) at 15,000 feet (4,572 meters). The Warhawk had a service ceiling of 30,600 feet (9,327 meters) and the absolute ceiling was 31,600 feet (9,632 meters). The range was 950 miles (1,529 kilometers) at 250 miles per hour (402 kilometers per hour).
Captain Charles W. Stark, Jr., 35th Pursuit Squadron, 8th Pursuit Group, climbing from the cockpit of a Curtiss-Wright P-40 Warhawk, 39-188, at Langley, Field, Virginia, 1941. Note the single .30-caliber machine gun visible on the left wing. (Rudy Arnold Collection/NASM)
The fighter (at the time, the Air Corps designated this type as a “pursuit”) was armed with two air-cooled Browning AN-M2 .50-caliber machine guns on the engine cowl, synchronized to fire through the propeller, with 380 rounds of ammunition per gun. Provisions were included for one Browning M2 .30-caliber aircraft machine gun, with 500 rounds of ammunition, in each wing.
The first production P-40 Warhawk, 39-156, made its first flight 4 April 1940. The 8th Pursuit Group at Langley Field, Virginia, was the first Army Air Corps unit to be equipped with the P-40.
Curtiss-Wright P-40 Warhawks of the 8th Pursuit Group at Langley Field, Virginia, 1940. (Unattributed)
After 200 P-40s were produced for the Air Corps, production was interrupted to allow Curtiss-Wright to build 100 Hawk 85A-1 export variants for the French Armée de l’air, then engaged with the invading forces of Nazi Germany. When France surrendered 22 June 1940, none of these airplanes had been delivered. The order was then assumed by the British Royal Air Force as the Tomahawk I.
U.S. Warhawk production resumed as the improved P-40B, and the remainder of the P-40 order was cancelled.
Second-Lieutenant William Barnard Rhodes-Moorhouse, Royal Flying Corps (Beaminster Museum)
War Office,
22nd May, 1915.
His Majesty the KING has been graciously pleased to approve the grant of the Victoria Cross to the undermentioned Officers, Non-commissioned officer, and Men, for their conspicuous acts of bravery and devotion to duty whilst serving with the Expeditionary Force :—
2nd Lieutenant William Barnard Rhodes-Moorhouse, Special Reserve, Royal Flying Corps.
For most conspicuous bravery on 26th April, 1915, in flying to Courtrai and dropping bombs on the railway line near that station. On starting the return journey he was mortally wounded, but succeeded in flying for 35 miles to his destination, at a very low altitude, and reported the successful accomplishment of his object. He has since died of his wounds.
—The London Gazette, Special Supplement 29170, Saturday, 22 May, 1915 at Pages 4989–4990
Chlorine gas dispersing downwind at the Second Battle of Ypres, 22 April 1915.
Beginning 22 April 1915 at the Second Battle of Ypres, the military forces of the German Empire began to use lethal chlorine gas as a weapon on the battlefield. A second mass gas attack took place on 24 April.
The Royal Flying Corps was ordered to interdict the German supply lines by bombing railways. On 26 April 1915, Second-Lieutenant William Barnard Rhodes-Moorhead, Royal Flying Corps, of No. 2 Squadron at Merville, France, was assigned to attack the railway at Kortrijk, West Floandern (Courtrai, West Flanders) with his Royal Aircraft Factory B.E.2.b reconnaissance airplane, number 687.
Departing alone from Merville at 3:05 p.m., Lieutenant Rhodes-Moorhouse flew to his target, approximately 35 miles (56 kilometers) away. He approached the railway station from an altitude of approximately 300 feet (91 meters) to accurately drop his single 100 pound (45.4 kilogram) bomb. He was hit in a leg by a rifle bullet, and shrapnel from his bomb damaged his airplane.
As Rhodes-Moorhouse flew away from the railroad station, he descended to 200 feet (61 meters) and was wounded twice more.
Gare de Kortrijk (the Courtrai Railroad Station)
The wounds to his hand and leg were serious, but the one to his abdomen was mortal. However, he continued the difficult return flight in his damaged airplane, and arrived back at Merville at 4:12 p.m. Rhodes-Moorhouse’ airplane had 95 holes from bullets and shrapnel. The wounded pilot insisted on making a report to his commanding officer and friend, Captain Maurice Bernal Blake, before being taken to an aid station.
It was soon apparent that Rhodes-Moorhouse would not survive. Captain Blake informed him that he had recommended that he be awarded the Distinguished Service Order.
Second-Lieutenant William Barnard Rhodes-Moorhouse, No. 2 Squadron, Royal Flying Corps, died of wounds at 2:25 p.m., 27 April 1915.
He was awarded the Victoria Cross, the United Kingdom’s highest award for valor, on 22 May 1915. Lieutenant Rhodes-Moorhouse was the first airman of the British Empire to be so decorated.
His medal is part of the Lord Ashcroft Victoria Cross Collection, displayed in the Aschcroft Gallery of the Imperial War Museum. He also was awarded the 1914–1915 Star, The British War Medal 1914–1918, and the Allied Victory Medal.
Field Marshal John Denton Pinkstone French, 1st Earl of Ypres, K.P., G.C.B., O.M., G.C.V.O., K.C.M.G., A.D.C., P.C., commanding general of the British Expeditionary Force, later said that Lieutenant Rhodes-Moorhouse had been responsible for “the most important bomb dropped during the war so far.”
Rhodes-Morehouse’ remains were buried at the family home at Parnham Park,¹ Beaminster, Dorset. After his son, Flight Lieutenant William Henry Rhodes-Morehouse, D.F.C., No. 601 Squadron, was killed when his Hawker Hurricane was shot down during the Battle of Britain, his ashes were placed alongside his father.
William Bernard Rhodes-Moorhouse
William Barnard Rhodes-Moorhouse was born into a wealthy family at 15 Princes Gate, London, England, 26 September 1887. He was one of four children of Edward Moorhouse, “a gentleman of independent means,” and Mary Ann Rhodes, the wealthiest woman in New Zealand. Moorhouse was educated Harrow School in northwest London, and Trinity College, Cambridge.
Radley monoplane on Portholme meadow. Constructed in 1911 in the Old Iron Foundry, St.John’s Street, H’don. Copyright – Huntingdon Record Office
Moorhouse developed an early interest in aviation and was soon an expert airman of international renown. Working with James Radley at Huntingdon, he developed the Radley-Moorhouse Monoplane. In 1910, Radley and Moorhouse traveled to the United States to demonstrate their airplane. Moorhouse is reportedly the first person to have flown through San Francisco’s Golden Gate. He was granted pilot’s certificate No. 147 by the Royal Aero Club of the United Kingdom, 17 October 1911.
In 1912, Moorhouse legally changed his surname to Rhodes-Moorhouse (and thereby replaced his second middle name, or maternal surname, Rhodes), because of the terms of his grandfather’s will. A Royal Licence authorizing the change was granted 11 January 1913, and published in The London Gazette ten days later.²
Mr. and Mrs. Rhodes-Moorhouse, 25 June 1912. (The Bowes Museum’s Blog)
Rhodes-Moorhouse married Miss Linda Beatrice Morrit at St. Paul’s, Knightsbridge, 25 June 1912, . They had one son, William Henry Rhodes-Moorhouse, born in 1914.
Mr. and Mrs. Rhodes-Moorhouse, along with John Henry Ledeboer, crossed the English Channel on 4 August 1912 in a three-place Société des Ateliers d’Aviation Louis Breguet 3-place biplane, flying from Douai, in northern France, where the airplane was built, to Ashwood, Staffordshire, England. The airplane was destroyed in a crash landing, but no one was hurt.
A Breguet 3-place biplane, 1912. (FLIGHT)
With England drawn into World War I, Rhodes-Moorhouse joined the Royal Flying Corps, 24 August 1914, and was assigned to the Royal Aircraft Factory at Farnborough. He was transferred to No. 2 Squadron, joining the unit at Merrville on 21 March 1915. He died just over one month later.
Royal Aircraft Factory B.E.2
The Royal Aircraft Factory B.E. (which stands for Blériot Experimental, meaning that it was a tractor-type airplane, which had been developed by Louis Blériot) was designed by Geoffrey de Havilland. It was a two-place, single-engine, two-bay biplane which was used as a trainer, reconnaissance aircraft, artillery spotter or bomber. An observer occupied the forward cockpit and the pilot was aft.
The B.E.2.b was essentially the same as the B.E.2.a, except the cockpit sides were higher. The elevator control cables were external from the pilot’s cockpit, aft. Probably the most significant change was the use of ailerons for the B.E.2.b, where the previous versions had used wing-warping like the original 1903 Wright Flyer.
The fuselage was constructed of a wooden framework, cross-braced with wires. The wings had wood spars and ribs. The airframe was covered in doped fabric.
The wings of the 2.a and 2.b were straight with no dihedral. Both upper and lower wings had the same span and there was no stagger. The lower wing spars were connected through the fuselage with steel tubing. The landing gear had both wheels and tires, but also wood-covered steel tube skids extending forward to protect the propeller from contacting the ground.
This Royal Aircraft Factory B.E.2.a, No. 347, of No. 2 Squadron, Royal Flying Corps, at Lythe, near Whitby, North Yorkshire, June 1914. Its pilot, Lieutenant Hubert Dunsterville Harvey-Kelly, Royal Irish Regiment, is at the lower right of the photograph. (Imperial War Museum Image number Q 54985)
The B.E.2.a–2.b was 29 feet, 6½ inches (9.004 meters) long with a wingspan of 38 feet, 7½ inches (11.773 meters). It had an empty weight of 1,274 pounds (578 kilograms) and gross weight of 1,650 pounds (748 kilograms).
The B.E.2, B.E.2.a and B.E.2.b were powered by an air-cooled, normally-aspirated 6.949 liter (424.036 cubic inch) Renault Type WB side-valve 90° V-8 engine with two valves per cylinder and a compression ratio of 4.12:1. The WB was rated at 70 horsepower at 1,750 r.p.m. The engine drove a four-bladed, fixed-pitch wooden propeller at one-half crankshaft speed. The Renault WB was 3 feet, 9.5 inches (1.556 meters) long, 2 feet, 8.8 inches (0.833 meters) high and 2 feet, 5.8 inches (0.757 meters) wide. It weighed 396 pounds (180 kilograms).
Armstrong Whitworth B.E.2.c, s/n 1799. Compare the staggered wings to those of the the B.E.2.a. in the photograph above.
The airplane had a maximum speed of 70 miles per hour (113 kilometers per hour) at Sea Level and 65 miles per hour (105 kilometers per hour) at 6,500 feet (1,981 meters). It could climb to 3,000 feet (914 meters) in 9 minutes and 7,000 feet (2,134 meters) in 35 minutes. The service ceiling was 10,000 feet (3,048 meters). Maximum endurance was 3 hours.
The B.E.2.b was unarmed. The crew could only defend themselves with their personal weapons. The type was easy prey for German fighters. It could carry a small bomb.
Although designed by the Royal Aircraft Factory, Farnbourough, only 6 B.E.2s were built there. The remainder were built by Armstong Whitworth, British and Colonial Airplane Co., Coventry Ordnance Works, Handley Page, Hewlett and Blondeau, and Vickers. Eighty-five of the B.E.2.b variant were produced, with most being used as trainers. Nineteen were sent to the Expeditionary Force in France, and one to the Middle East Brigade. By late 1915, the type had been almost completely replaced by the improved B.E.2.c.
A reproduction of the Royal Aircraft Factory B.E.2.b flown by Lieutenant Rhodes-Moorhouse is in the collection of the Royal Air Force Museum. In a 2015 interview with Richard Moss for “Culture 24,” Ian Thirsk, Head of Collections, said, “It’s another gem of the collection, and was built from scratch by a designer called John McKenzie to the original drawings at the former RAF Museum facility at Cardington between 1983 and 1988.”
Reproduction of 2nd Lieutenant W.B. Rhodes-Moorhouse’ Royal Aircraft Factory B.E.2.b, No. 687, at the Royal Air Force Museum, Hendon. (British Aviation Preservation Council)
¹ Interestingly, Parnham House is believed to have been the inspiration for Sir Arthur Conan Doyle’s “Baskerville Hall” in his famous novel, The Hound of the Baskervilles (1902).
Parnham House, East Front. William Barnard Rhodes-Moorhouse’ home in Dorset, England. (Country Life Magazine, 29 August 1908)
² The London Gazette, Number 28683, Tuesday, 21 January 1913, at Page 494, Column 1
A McDonnell Douglas Helicopter Company MD530F. This is the same type helicopter flown by Jack Schweibold to set an FAI world speed record, 25 April 1985. (Rotor Hub)
25 April 1985: Flying a McDonnell Douglas Helicopter Company MD530F, Allison Chief Test Pilot Frederick Jack Schweibold sets a Fédération Aéronautique Internationale (FAI) world record for speed over a recognized course from Kansas City, Missouri, to Indianapolis, Indiana, at an average speed of 276,12 kilometers per hour (171.573 miles per hour).¹
The MD530F (Model 369FF) is the most powerful variant of the Model 369 series, which was originally produced by Hughes Helicopters as the military OH-6A Cayuse Light Observation Helicopter. It is optimized for “hot and high” operations. It has longer main rotor blades than the MD500E, and is powered by an Allison 250-C30 turboshaft engine. The helicopter is now produced by MD Helicopters, Mesa, Arizona.
MD530F three-view illustration with dimensions from sales brochure. (MD Helicopters)
Lieutenant Colonel Frank K. Everest, U.S. Air Force, with a Bell X-2 at Edwards Air Force Base. Colonel Everest is wearing a David Clark Co. T-1 capstan-type partial-pressure suit for protection at very high altitude. (U.S. Air Force)
25 April 1956: At Edwards Air Force Base, California, test pilot Lieutenant Colonel Frank Kendall (“Pete”) Everest, United States Air Force, was airdropped from a Boeing EB-50D Superfortress in the Bell X-2 supersonic research rocket plane, serial number 46-674. This was the tenth flight of the X-2 program, and only the third powered flight.
For the first time, Everest fired both chambers of the Curtiss-Wright XLR25 rocket engine. On this flight, the X-2 reached Mach 1.40 and 50,000 feet (15,240 meters). It was the first time an X-2 had gone supersonic.
Bell X-2 46-674 in flight over Southern California, circa 1955–56. (NASA Photograph ET–128)
The X-2 was a joint project of the U.S. Air Force and NACA (the National Advisory Committee on Aeronautics, the predecessor of NASA). The rocketplane was designed and built by Bell Aircraft Corporation of Buffalo, New York, to explore supersonic flight at speeds beyond the capabilities of the earlier Bell X-1 and Douglas D-558-II Skyrocket.
In addition to the aerodynamic effects of speeds in the Mach 2.0–Mach 3.0 range, engineers knew that the high temperatures created by aerodynamic friction would be a problem, so the aircraft was built from stainless steel and K-Monel, a copper-nickel alloy.
The Bell Aircraft Corporation X-2 was 37 feet, 10 inches (11.532 meters) long with a wingspan of 32 feet, 3 inches (9.830 meters) and height of 11 feet, 10 inches (3.607 meters). Its empty weight was 12,375 pounds (5,613 kilograms) and loaded weight was 24,910 pounds (11,299 kilograms).
The X-2 was powered by a throttleable two-chamber Curtiss-Wright XLR25-CW-1 rocket engine that produced 2,500–15,000 pounds of thrust (11.12–66.72 kilonewtons).
Rather than use its limited fuel capacity to take off and climb to altitude, the X-2 was dropped from a modified heavy bomber as had been the earlier rocketplanes. A four-engine Boeing B-50D-95-BO Superfortress bomber, serial number 48-096, was modified as the drop ship and redesignated EB-50D.
Bell X-2 46-674 on final approach. (NASA)
The launch altitude was 30,000 feet (9,144 meters). After the fuel was exhausted, the X-2 glided to a touchdown on Rogers Dry Lake at Edwards Air Force Base.
Two X-2 rocketplanes were built. The second X-2, 46-675, was destroyed during a captive flight, 12 May 1953. The explosion killed Bell test pilot Skip Ziegler and Frank Wolko, an engineer aboard the B-50A mothership. The B-50 made an emergency landing but was so badly damaged that it never flew again.
The X-2 reached a maximum speed of Mach 3.196 (2,094 miles per hour/3,370 kilometers per hour) and maximum altitude of 126,200 feet (38,466 meters).
Boeing EB-50D Superfortress 48-096 with a Bell X-2 (U.S. Air Force)
The EB-50D was a highly modified four-engine Boeing B-50D-95-BO Superfortress long range heavy bomber, engineered to carry research aircraft to high altitudes before releasing them for a test flight. The B-50 was an improved version of the World War II B-29A Superfortress.
Boeing B-50D-95-BO (S/N 48-096) in flight. (U.S. Air Force photo)Boeing B-50D-95-BO Superfortress 48-096 prior to modification to an EB-50D X-2 carrier. (U.S. Air Force/Bill Pippin Collection, 1000aircraftphotos.com)Boeing B-50D-95-BO Superfortress 48-096 prior to modification to an EB-50D X-2 carrier. (U.S. Air Force)Boeing B-50D-95-BO Superfortress 48-096 prior to modification to an EB-50D X-2 carrier. (U.S. Air Force)
Frank Kendall (“Pete”) Everest, Jr., was born 10 Aug 1920, at Fairmont, Marion County, West Virginia. He was the first of two children of Frank Kendall Everest, an electrical contractor, and Phyllis Gail Walker Everest. Attended Fairmont Senior High School, Fairmont, West Virginia, graduating in 1939. He studied at Fairmont State Teachers College, also in Fairmont, West Virginia, and then studied engineering at teh University of Wesst Virginia in Morgantown.
Pete Everest enlisted as an aviation cadet in the United States Army Air Corps at Fort Hayes, Columbus, Ohio, 7 November 1941, shortly before the United States entered World War II. His enlistment records indicate that he was 5 feet, 7 inches (1.703 meters) tall and weighed 132 pounds (59.9 kilograms). He graduated from pilot training and was commissioned as a second lieutenant, Air Reserve, 3 July 1942.
Everest married Miss Avis June Mason in Marion, West Virginia, in 1942.
Pete Everest with his Curtiss-Wright P-40 Warhawk, North Africa, 1943.
He was promoted to 1st Lieutenant, Army of the United States, 11 November 1942. He was assigned as a Curtiss-Wright P-40 Warhawk pilot, flying 94 combat missions in North Africa, Sicily and Italy. He was credited with shooting down two German airplanes and damaging a third. Everest was promoted to the rank of Captain, 17 August 1943.
In 1944, Everest was returned to the United States to serve as a flight instructor. He requested a return to combat and was then sent to the China-Burma-India theater of operations where he flew 67 missions and shot down four Japanese airplanes. He was himself shot down by ground fire in May 1945. Everest was captured by the Japanese and suffered torture and inhumane conditions before being freed at the end of the war. He was promoted to the rank of major, 1 July 1945. He was returned to the United States military 3 October 1945.
After the war, Everest was assigned as a test pilot at Wright-Patterson Air Force Base, Ohio, before going west to the Air Force Flight Test Center at Edwards Air Force Base, California.
Everest was returned to the permanent rank of first lieutenant, Air Corps, 19 June 1947, with date of rank retroactive to 3 July 1945.
Major Frank Kendall Everest, Jr., U.S. Air Force, with a Bell X-1 supersonic research rocketplane, 46-062, circa 1950. (mach-buster.co.uk)
At Edwards, he was involved in nearly every flight test program, flying the F-88, F-92, F-100, F-101, F-102, F-104 and F-105 fighters, the XB-51, YB-52, B-57 and B-66 bombers. He also flew the pure research aircraft, the “X planes:” the X-1, X-1B, X-2, X-3, X-4 and X-5. Pete Everest flew the X-1B to Mach 2.3, and he set a world speed record with the X-2 at Mach 2.9 (1,957 miles per hour, 3,149.5 kilometers per hour) which earned him the title, “The Fastest Man Alive.” He was the test pilot on thirteen of the twenty X-2 flights.
Major Frank Kendall Everest, Jr., U.S. Air Force, with the Bell X-2 supersonic research rocketplane, on Rogers Dry Lake at Edwards AFB, California, 1956. (U.S. Air Force via Jet Pilot Overseas)
Frank Everest returned to operational assignments and commanded a fighter squadron, two combat crew training wings, and was assigned staff positions at the Pentagon. On 20 November 1963, Colonel Everest, commanding the 4453rd Combat Crew Training Squadron, flew one of the first two operational McDonnell F-4C Phantom II fighters from the factory in St. Louis to MacDill Air Force Base.
Brigadier General Gilbert L. Meyers and Colonel Frank Kendall Everest delivered the first production F-4C Phantom IIs to the Tactical Air Command at MacDill Air Force Base, Florida. (U.S. Air Force)
In 1965, Pete Everest was promoted to the rank of brigadier general. He was commander of the Aerospace Rescue and Recovery Service. He retired from the Air Force in 1973 after 33 years of service. He later worked as a test pilot for Sikorsky Aircraft.
During his military career General Everest was awarded the Air Force Distinguished Service Medal; Legion of Merit with two oak leaf clusters (three awards); Distinguished Flying Cross with two oak leaf clusters (three awards); Purple Heart; Air Medal with one silver and two bronze oak leaf clusters (seven awards); Air Force Commendation Medal with one oak leaf cluster (two awards); Presidential Unit Citation with two bronze oak leaf clusters (three awards); Air Force Gallant Unit Citation; Prisoner of War Medal; American Campaign Medal; European-African-Middle Eastern Campaign medal with four bronze stars; Asiatic-Pacific campaign Medal with two bronze stars; World War II Victory Medal; National Defense Service Medal; Armed Forces Expeditionary Medal; Vietnam Service Medal; Air Force Longevity Service Award with one silver and two bronze oak leaf clusters (seven awards); Air Force Small Arms Expert Marksmanship Ribbon; and the Republic of Vietnam Campaign Medal with 1960– device. General Everest was rated as a Command Pilot, and a Basic Parachutist.
Brigadier General Frank Kendall Everest, Jr. United States Air Force (Retired), died at Tucson, Arizona, 1 October 2004 at the age of 84 years.
Brigadier General Frank Kendall Everest, Jr., United States Air Force. (U.s. Air Force)
Aviation Cadet Raymond L. Knight, United States Army Air Corps. (U.S. Air Force)
MEDAL OF HONOR
RAYMOND L. KNIGHT
Rank and organization: First Lieutenant, U.S. Army Air Corps.
Place and date: In Northern Po Valley, Italy, 24-25 April 1945.
Entered service at: Houston, Texas. Born: Texas.
G.O. No.: 81, 24 September 1945.
Medal of Honor
Citation: First Lieutenant Raymond L. Knight on 24 and 25 April 1945 in the northern Po Valley, Italy, piloted a fighter-bomber aircraft in a series of low-level strafing missions, destroying 14 grounded enemy aircraft and leading attacks which wrecked 10 others during a critical period of the Allied drive in northern Italy. On the morning of 24 April, he volunteered to lead two other aircraft against the strongly defended enemy airdrome at Ghedi. Ordering his fellow pilots to remain aloft, he skimmed the ground through a deadly curtain of antiaircraft fire to reconnoiter the field, locating eight German aircraft hidden beneath heavy camouflage. He rejoined his flight, briefed them by radio, and then led them with consummate skill through the hail of enemy fire in a low-level attack, destroying five aircraft, while his flight accounted for two others. Returning to his base, he volunteered to lead three other aircraft in reconnaissance of Bergamo Airfield, an enemy base near Ghedi and one known to be equally well defended. Again ordering his flight to remain out of range of antiaircraft fire, Lieutenant Knight flew through an exceptionally intense barrage, which heavily damaged his Thunderbolt, to observe the field at minimum altitude. He discovered a squadron of enemy aircraft under heavy camouflage and led his flight to the assault. Returning alone after this strafing, he made 10 deliberate passes against the field despite being hit twice more by antiaircraft fire, destroying six fully loaded enemy twin-engine aircraft and two fighters. His skillfully led attack enabled his flight to destroy four other twin-engine aircraft and a fighter airplane. He then returned to his base in his seriously damaged airplane. Early the next morning, when he again attacked Bergamo, he sighted an enemy plane on the runway. Again he led three other American pilots in a blistering low-level sweep through vicious antiaircraft fire that damaged his airplane so severely that it was virtually nonflyable. Three of the few remaining enemy twin-engine aircraft at that base were destroyed. Realizing the critical need for aircraft in his unit, he declined to parachute to safety over friendly territory and unhesitatingly attempted to return his shattered airplane to his home field. With great skill and strength, he flew homeward until caught by treacherous air conditions in the Apennine Mountains, where he crashed and was killed. The gallant action of Lieutenant Knight eliminated the German aircraft which were poised to wreak havoc on Allied forces pressing to establish the first firm bridgehead across the Po River. His fearless daring and voluntary self-sacrifice averted possible heavy casualties among ground forces and the resultant slowing of the drive which culminated in the collapse of German resistance in Italy.
1st Lieutenant Raymond L. Knight with a battle-damaged Republic P-47D Thunderbolt fighter bomber. (U.S. Air Force)
Raymond Larry Knight was born 15 June 1922 in Houston, Texas. He was the third child of John Franklin Knight, a clerk, and Sarah Francis Kelly Knight. He attended John H. Reagan Senior High School in Houston, graduating in 1940.
Knight married Miss Johnnie Lee Kinchloe, also a 1940 graduate of Reagan High School, 5 June 1942. They had one son, Raymond Jr.
Knight enlisted as an aviation cadet in the United States Army Air Corps, 10 Oct 1942, and trained as a fighter pilot at various airfields in Texas. He graduated from flight school and was commissioned as a second lieutenant, May 1944. After advanced training, Knight was assigned to the 346th Fighter Squadron, 350th Fighter Group, 12th Air Force, at Tarquinia Airfield, Italy, in November 1944. He was promoted to first lieutenant in March 1945.
Lieutenant Knight flew 82 combat missions. He is credited with 14 enemy aircraft destroyed.
The Medal of Honor was presented to Mrs. Knight by Major General James Pratt Hodges at a ceremony at John H. Reagan Senior High School, 23 October 1945.
In addition to the Medal of Honor, Lieutenant Knight was also awarded the Distinguished Flying Cross, and the Air Medal with five oak leaf clusters (six awards).
The remains of 1st Lieutenant Raymond Larry Knight, United States Army Air Corps, are interred at the Houston National Cemetery, Houston, Texas.
1st Lieutenant Raymond L. Knight (at right) and crew chief Sergeant Marvin Childers, with Republic P-47D-27-RE Thunderbolt 42-26785, marked 6D5. This is the fighter bomber that he flew on the final mission. It was named “OH JOHNNIE” after his wife. (U.S. Air Force)
The Republic P-47 Thunderbolt was the largest single-engine fighter that had yet been built. The first P-47D variant was very similar to the preceding P-47C. The Thunderbolt which Raymond Knight flew on his final mission was a P-47D-27-RE, serial number 42-26785. He had named it OH JOHNNIE after his wife. The Thunderbolt’s bubble canopy had been introduced with the Block 25 series, and Block 27 added a dorsal fillet to improve longitudinal stability which had been diminished with the new aft fuselage configuration.
The P-47D-27-RE was 36 feet, 1¾ inches (11.017 meters) long with a wingspan of 40 feet, 9-3/8 inches (12.430 meters) The overall height was 14 feet, 7 inches (4.445 meters). The fighter’s empty weight was 10,700 pounds (4,853 kilograms) and maximum gross weight was 17,500 pounds (7,938 kilograms).
The P-47D-27-RE was powered by an air-cooled, supercharged and turbocharged 2,804.4-cubic-inch-displacement (45.956 liter) Pratt & Whitney Double Wasp TSB1-G (R-2800-59) two-row, 18-cylinder radial engine with a compression ratio of 6.65:1. The R-2800-59 had a Normal Power rating of 1,625 horsepower at 2,550 r.p.m. to 25,000 feet (7,620 meters) and a Takeoff/Military Power rating of 2,000 horsepower at 2,700 r.p.m. to an altitude of 25,000 feet (7,620 meters).¹ A large General Electric turbosupercharger was mounted in the rear of the fuselage. Internal ducts carried exhaust gases from the engine to drive the turbocharger. This supercharged air was then carried forward through an intercooler and then on to the carburetor to supply the engine. The engine’s mechanical supercharger further pressurized the air-fuel charge. The engine drove a 13 foot, 0 inch (3.962 meter) diameter four-bladed Curtiss Electric or Hamilton Standard Hydromatic propeller through a 2:1 gear reduction. The R-2800-59 was 6 feet, 3.72 inches (1.923 meters) long, 4 feet, 4.50 inches (1.340 meters) in diameter, and weighed 2,290 pounds (1,039 kilograms).
A flight of three Republic P-47 Thunderbolt fighters. (U.S. Air Force)
The P-47D had a maximum speed in level flight of 444 miles per hour (715 kilometers per hour) at 23,200 feet (7,071 meters) with 70 inches Hg manifold pressure (2.37 Bar), using water injection. The service ceiling was 40,000 feet (12,192 meters). It had a maximum range of 950 miles (1,529 kilometers) with internal fuel, and 1,800 miles (2,897 kilometers) with external tanks.
The Thunderbolt was armed with eight Browning AN-M2 .50-caliber machine guns, four in each wing, with 3,400 rounds of ammunition. It could also carry external fuel tanks, rockets and bombs. The structure of the P-47 could be described as “robust” and it was heavily armored. The amount of damage that the airplane could absorb and still return was remarkable.
A total of 15,683 Thunderbolts were built; more than any other Allied fighter type. In aerial combat, it had a kill-to-loss ratio of 4.6:1. The P-47, though, really made its name as a ground attack fighter, destroying aircraft, locomotives, rail cars, and tanks by the many thousands. It was one of the most successful aircraft of World War II.
¹ A rebuilt R-2800-63 was run at War Emergency Power (2,600 horsepower at 2,700 r.p.m.) for 7½ hours on a test stand, and was in running condition when the test was completed.
The Curtiss-Wright Corporation Hawk 81 (P-40 Warhawk) was a single-seat, single-engine pursuit, designed by Chief Engineer Donovan Reese Berlin. It was developed from Berlin’s radial-engine P-36 Hawk. The P-40 was a low-wing monoplane of all-metal construction and used flush riveting to reduce aerodynamic drag. It had an enclosed cockpit and retractable landing gear (including the tail wheel). Extensive wind tunnel testing at the NACA Langley laboratories refined the airplane’s design, significantly increasing the top speed.
The P-40 was powered by a liquid-cooled, supercharged, 1,710.597-cubic-inch-displacement (28.032 liter) Allison Engineering Co. V-1710-C15 (V-1710-33). This was a single overhead cam (SOHC) 60° V-12 engine designed by Harold Caminez, Allison’s chief engineer. The V-1710-33 had a compression ratio of 6.65:1. It was rated at 930 horsepower at 2,600 r.p.m. at 12,800 feet (3,901 meters), and 1,040 horsepower at 2,800 r.p.m. for takeoff, burning 100-octane gasoline. The engine turned a three-bladed Curtiss Electric constant-speed propeller through a 2:1 gear reduction. The V-1710-33 was 8 feet, 2.54 inches (2.503 meters) long, 3 feet, 5.88 inches (1.064 meters) high, and 2 feet, 5.29 inches (0.744 meters) wide. It weighed 1,340 pounds (607.8 kilograms).
