19 March 1945

Pilot Officer P. Martin's Avro Lancaster B Mk.I Special, PB996, YZ-C, releases the 22,000-pound Grand Slam earth-penetrating bomb over teh railway viaduct at Arnsberg, Germany, 19 March 1945. (Imperial War Museum)
Pilot Officer P. Martin’s Avro Lancaster B Mk.I Special, PB996, YZ-C, releases the 22,000-pound Grand Slam earth-penetrating bomb over the railway viaduct at Arnsberg, Germany, 19 March 1945. © IWM (CH 15735)
The Grand Slam bomb drops away from the No. 617 Squadron Lancaster B Mk.I Special, YZ-C, 19 March 1945. (Imperial War Museum)
The Grand Slam bomb drops away from the No. 617 Squadron Lancaster B Mk.I Special, YZ-C, 19 March 1945. © IWM (CH 15374)

19 March 1945: Modified Avro Lancaster B Mk.I Special heavy bombers of No. 617 Squadron, Royal Air Force, attacked the railway viaduct at Arnsberg, Germany, using the 22,000 pound (9,979 kilogram) Grand Slam earth-penetrating bomb. The bomb had been first used just days before, 14 March, against another railway viaduct.

The Grand Slam was the largest and heaviest aerial bomb used during World War II. It was designed by aircraft engineer Barnes Neville Wallis, and was scaled up from his earlier, smaller “Tallboy.” (Wallis also designed the “Upkeep” Special Mine used to attack hydroelectric dams in the Ruhr Valley in 1943.)

The Grand Slam bomb dropped by Flying Officer Martin's Avro Lancaster exploeds underneath the railway viaduct at Arnsberg, Germany. (Imperial War Museum)
The Grand Slam bomb dropped by Flying Officer Martin’s Avro Lancaster explodes underneath the railway viaduct at Arnsberg, Germany. Bomb craters from previous unsuccessful attacks are visible in this RAF photograph. © IWM (CH 15378)

Wallis’ idea was that a very heavy, supersonic bomb could penetrate deep into the earth and detonate, causing an “earthquake” which could destroy nearby heavily protected targets.

Tall Boy and Grand Slam Deep Penetration Bombs (British Explosive Ordnance, Part 1, Chapter 7)

The Grand Slam bomb (officially, “Bomb, D.P., 22,000-lb., Mk I”) was 25 feet, 5 inches (7.747 meters) long and had a maximum diameter of 3 feet, 10 inches (1.168 meters). When fully loaded with the explosive material, Torpex, the bomb weighed 22,400 pounds (10,160 kilograms).

Completed bomb casings for Barnes Wallis’ 22,000-pound “Grand Slam” deep penetration bomb, photographed 7 January 1945. The individual weight is stenciled on each casing. (Tyne & Wear Archives)

The bomb case was cast of steel at the Clyde Alloy and Steel Company, Glasgow, Scotland, then, after several days of cooling, machined to its precise shape. The casing made up approximately 60% of the bomb’s total weight. At the nose, the casing had a wall thickness of 7.75 inches (19.685 centimeters).

A "Bomb, Medium Capacity, 22,000 Pounds, lifted by a crane at a Royal Air Force bomb dump. (Imperial War Museum)
A “Bomb, Deep Penetration, 22,000 Pounds”—the Grand Slam—lifted by a crane at a Royal Air Force bomb dump. © IWM (CH 15369)

The bomb case was filled with approximately 9,200 pounds (4,173 kilograms) of molten Torpex, with a 1 inch (2.54 centimeters) topping of TNT. Torpex was an explosive designed for torpedo warheads and depth charges. It was made up of approximately equal quantities of two other explosives, Research Department Formula X (RDX), 42%, and trinitrotoluol (TNT), 40%, mixed with 18% powdered aluminum and wax. The resulting combination was approximately 1.4 times more powerful than TNT alone. About one month was required for the explosive to cool after being poured into the bomb case.

Because of its size and weight, the only Allied bomber capable of carrying the Grand Slam was a specially modified Avro Lancaster B.I Special, flown by No. 617 Squadron, Royal Air Force, “The Dambusters.”

An Avro Lancaster very long range heavy bomber carrying a Gland Slam bomb. (Royal Air Force)

Wallis intended for the Grand Slam to be dropped from very high altitudes so that during its fall, it would go supersonic. The bomb had large fins that were offset 5° to the right of the centerline to cause it to rotate for stability. However, the bombers could not carry it to the planned release altitude, and it was typically dropped from approximately 9,000 feet (2,743 meters). Its very sleek design did allow it to come close to the speed of sound, however, and its stability made it a very accurate weapon. The bomb was capable of penetrating 20-foot-thick (6 meters) reinforced concrete roofs of submarine bases. ¹

Arnsberg railway viaduct following Grand Slam bombing attack. (Royal Air Force)

Barnes Neville Wallis, Esq., M. Inst. C.E., F.R.Ae.S., Assistant Chief Designer Vickers-Armstrongs Ltd., was appointed Commander of the Most Excellent Order of the British Empire (Civil Division), by His Majesty, King George VI, 2 June 1943.

Sir Barnes Neville Wallis C.B.E., was knighted by Her Majesty, Queen Elizabeth II, 13 December 1968.

Sir Barnes Neville Wallis C.B.E.

¹ “The striking velocity of the bomb, when released at an altitude of 16,000 ft. and an air speed of 200 m.p.h., is stated at 1,097 ft./sec., at which speed it has developed a rotational velocity of 60 r.p.m.” —British Explosive Ordnance, Part 1, Chapter 7

© 2019, Bryan R. Swopes

19 March 1937

Amelia Earhart's Lockheed Electra 10E Special, NR16020, in a hangar at Wheeler Field, Honolulu, Territory of Hawaii, 19 March 1937. (Hawaii's Aviation History, http://hawaii.gov/hawaiiaviation )
Amelia Earhart’s Lockheed Electra 10E Special, NR16020, in a hangar at Wheeler Field, Honolulu, Territory of Hawaii, 19 March 1937. (Hawaii’s Aviation History)

19 March 1937: After her 15 hour, 47 minute, overnight flight from Oakland, California, Amelia Earhart’s Lockheed Electra 10E Special NR16020 was placed in a hangar at Wheeler Army Airfield, Honolulu, for maintenance and repair. During the flight, a propeller pitch change mechanism had failed. Inspection revealed that both propeller hubs were badly galled “due to improper or insufficient lubrication.” They were overhauled by the Army Air Corps’ Hawaiian Air Depot at Luke Field, then re-installed on the Electra.

At 11:15 a.m. on the 19th, Paul Mantz and two friends took the Electra for a test flight, then repositioned to Luke Field on Ford Island, with its longer, hard-surfaced runway, for an early morning takeoff on the second leg of the around-the-world flight.

Amelia Earhart's Lockheed Electra 10E Special, NR16020, with engines running at Wheeler Field, prior to repositioning to Luke Field, 19 March 1937. (Hawaii’s Aviation History, http://hawaii.gov/hawaiiaviation )
Amelia Earhart’s Lockheed Electra 10E Special, NR16020, with engines running at Wheeler Field, prior to repositioning to Luke Field, 19 March 1937. (Hawaii’s Aviation History)

© 2019, Bryan R. Swopes

18 March 1965

Voskhod-2/11A57 launch vehicle on launch pad at Site 1, Baikonur Cosmodrome (Space Facts)

18 March 1965, 07:00:00 UTC (10:00:00 Moscow Time): Cosmonauts Павел Иванович Беляев (Pavel Ivanovich Belyaev) and Алексей Архипович Леонов (Alexey Arkhipovich Leonov) were launched from the Baikonur Cosmodrome aboard a Voskhod-3KD spacecraft, Восход-2 (Voskhod-2). The launch vehicle was a Voskhod 11A57 two-stage liquid-fueled rocket. Voskhod-2 entered a 167 × 475 kilometers (90 × 256 nautical miles) elliptical orbit with a period of 90 minutes, 54 seconds.

As the Voskhod entered its second orbit, co-pilot Major Leonov exited the vehicle. An expandable air lock was used. This was the first time that a human had left a vehicle in space. He floated freely, though remained connected by an umbilical. This would be known as an Extravehicular Activity (an “E-V-A,” or “space walk”). Leonov remained outside for 12 minutes, 9 seconds, establishing the first FAI World Record for Extravehicular Duration in Space. ¹

Алексей Архипович Леонов (Alexey Arkhipovich Leonov) outside the Voskhod-2 spacecraft, 18 March 1965. (collectspace.com)

Both cosmonauts wore NPP Zvezda Berkut full-pressure suits (a “space suit”) for protection in the vacuum of space. With his suit fully inflated by pressurized air, Leonov was both larger and more rigid than was expected. He had great difficulty re-entering the Voskhod, requiring that he vent the suit pressure.

Leonov wrote about it for Air & Space:

With some reluctance I acknowledged that it was time to reenter the spacecraft. Our orbit would soon take us away from the sun and into darkness. It was then I realized how deformed my stiff spacesuit had become, owing to the lack of atmospheric pressure. My feet had pulled away from my boots and my fingers from the gloves attached to my sleeves, making it impossible to reenter the airlock feet first.

I had to find another way of getting back inside quickly, and the only way I could see to do this was pulling myself into the airlock gradually, head first. Even to do this, I would carefully have to bleed off some of the high-pressure oxygen in my suit, via a valve in its lining. I knew I might be risking oxygen starvation, but I had no choice. If I did not reenter the craft, within the next 40 minutes my life support would be spent anyway.

The only solution was to reduce the pressure in my suit by opening the pressure valve and letting out a little oxygen at a time as I tried to inch inside the airlock. At first I thought of reporting what I planned to do to mission control. But I decided against it. I did not want to create nervousness on the ground. And anyway, I was the only one who could bring the situation under control.

But I could feel my temperature rising dangerously high, with a rush of heat from my feet traveling up my legs and arms, due to the immense physical exertion all the maneuvering involved. It was taking longer than it was supposed to. Even when I at last managed to pull myself entirely into the airlock, I had to perform another almost impossible maneuver. I had to curl my body around in order to close the airlock, so pasha could activate the mechanism to equalize pressure between it and the spacecraft.

Once Pasha was sure the hatch was closed and the pressure had equalized, he triggered the inner hatch open and I scrambled back into the spacecraft, drenched with sweat, my heart racing.

“The Nightmare of Voskhod,” by Alexey Leonov, Air & Space Smithsonian, January 2005

Leonov  in the shadow of his spacecraft in orbit around the Earth, 18 March 1965. (collectspace.com)

On 19 March, Voshkod-2’s apogee set a Fédération Aéronautique Internationale (FAI) World Record for Altitude in Elliptical Orbit of 497,7 kilometers (268.7 nautical miles/309.3 statute miles). ²

The space craft began to lose pressure, with it’s oxygen tanks dropping by two-thirds during Orbit 13. It was thought that the mission might have to be cut short.

It was planned for Voskhod-2 to reenter on the 16th orbit, however the automatic landing system failed to fire the spacecraft’s retrorockets. Using the Voskhod’s primary engine, a manual reentry was initiated during the 18th orbit. The crew also had to orient the spacecraft manually, and this caused them a delay of 46 seconds before initiating reentry. They overshot their expected landing point by approximately 2,000 kilometers (1,250 miles).

Voshkod-2 landed in remote area of Perm Krai at 09:02:17 UTC on 19 March. The duration of the flight was 1 day, 2 hours, 2 minutes, 17 seconds.

Having landed in a dense forest hundreds of miles from the nearest recovery teams, Belyaev and Leonov were were located about four hours later and a rescue team arrived the next day. A landing zone was cut in the forest and the cosmonauts were flown out by helicopter on 21 March.

Voskhod-2 landed in dense forest. The cosmonauts were not recovered for two days.

¹ FAI Record File Number 9336

² FAI Record File Number 9335

© 2019, Bryan R. Swopes

18 March 1945

LaVerne Brown, Director of Flight Test, Douglas Aircraft Company, in the cockpit of the first XBT2D-1 Dauntless II prototype, Bu. No. 9085. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)
LaVerne Ward Browne, Director of Flight Test, Douglas Aircraft Company, in the cockpit of the first XBT2D-1 Dauntless II prototype, Bu. No. 9085. (Photograph courtesy of Neil Corbett, Test and Research Pilots, Flight Test Engineers)

18 March 1945: At the Naval Airplane Factory, El Segundo, California (at the southeast corner of Los Angeles Airport, now best known as LAX), Douglas Aircraft Company Director of Flight Test LaVerne Ward (“Brownie”) Browne took the prototype XBT2D-1 Dauntless II, Bu. No. 9085, for its first flight.

He later commented, “I wish I could tell of some dramatic incident that occurred. There wasn’t any. I just floated around up there for an hour and a half and brought her down. But I did do something that’s unprecedented, I believe, for a first trip. The airplane handled so well that I put it through rolls and Immelmanns to check it for maneuverability.”

The first prototype Douglas XBT2D-1 Dauntless II, Bu. No. 9085. In this photograph the airplane has a propeller spinner. (San Diego Air and Space Museum archive)
The first prototype Douglas XBT2D-1 Dauntless II, Bu. No. 9085. In this photograph the airplane has a propeller spinner. (Douglas Aircraft Company)

The XBT2D-1 would be ordered into production as the Douglas AD-1 Skyraider.

Designed by Douglas’ Chief Engineer, Edward Henry Heinemann, the XBT2D-1 was a single-place, single-engine attack bomber capable of operation from the U.S. Navy’s aircraft carriers. The prototype was 39 feet, 5 inches (12.014 meters) long with a wingspan of 50 feet, ¼ inch (15.246 meters) and overall height of 15 feet, 7½ inches (4.763 meters). The airplane had an empty weight of 10,093 pounds (4,578 kilograms) and maximum weight of 17,500 pounds (7,938 kilograms).

The first four XBT2D-1 prototypes were powered by an air-cooled, supercharged, 3,347.662-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division R3350-8 (Cyclone 18 779C18BB1) twin-row 18-cylinder radial engine rated at 2,100 horsepower at 2,400 r.p.m., and 2,400 horsepower at 2,600 r.p.m., for takeoff. The next 20 airplanes built utilized the R3350-24W (Cyclone 18 825C18BD1) which had a takeoff power rating of 2,500 horsepower at 2,900 r.p.m.

Both engines had a compression ration of 6.5:1 and a propeller drive reduction ratio of 0.4375:1. They differed in external dimensions and weight, with the –24W being both longer and heavier.

Test pilot Brown in teh cockpit of Douglas XBT2D-1 Dauntless II Bu. No. 9085 during a test flight. (Douglas Aircraft Company)
Test pilot LaVerne Brown in the cockpit of Douglas XBT2D-1 Dauntless II Bu. No. 9085 during a test flight. (Douglas Aircraft Company)

The XBT2D-1 had a maximum speed of 375 miles per hour (604 kilometers per hour) at 13,600 feet (4,145 meters) and normal cruise speed of 164 miles per hour (264 kilometers per hour).

The first XBT2D-1, Bu. No. 9085, was sent to NAS Patuxent River, Maryland, for further testing. The second, 9086, went to NACA Ames at Moffet Field, California, where it underwent testing from 11 March 1946 to 4 September 1947.

The second prototype XBT2D-1, Bu. No. 9086, was tested at the NACA Ames Research Center, Moffet Field, California, from 11 March 1946 to 4 September 1947. (NASA)
The second prototype XBT2D-1, Bu. No. 9086, at the NACA Ames Research Center, Moffet Field, California, 18 June 1946. (NASA)

3,180 Skyraiders in 11 variants were built at the Douglas Aircraft Company’s El Segundo, California, plant from 1945 to 1957. The attack bomber was widely used during the Korean War and the Vietnam War. It was utilized for many purposes but is best known for its close support missions during combat rescue operations. After 1962, the AD-series aircraft still in service were redesignated A-1E through A-1J.

Douglas XBT2D-1 Skyraider Bu. No. 9086 at NACA Ames Research Center, 18 June 1946. (NASA)

The most numerous Skyraider variant was the AD-6 (A-1H), of which 713 were produced by Douglas. The AD-6 was 38 feet, 10 inches (11.836 meters) long with a wingspan of 50 feet, 9 inches (15.469 meters) and overall height of 15 feet, 8¼ inches (4.782 meters). Its empty weight was 11,968 pounds (5,429 kilograms) and gross weight was 18,106 pounds (8,213 kilograms). The maximum takeoff weight (MTOW) for the AD-6 was 25,000 pounds (11,340 kilograms).

Douglas AD-4 Skyraider of VA-195 taking off from USS Princeton (CV-37) circa 1950–52 (U.S. Navy)
Douglas AD-4 Skyraider of VA-195 taking off from USS Princeton (CV-37) circa 1950–52 (U.S. Navy)

The Douglas AD-6 was powered by an air-cooled, supercharged, direct-fuel-injected, 3,347.662-cubic-inch-displacement (54.858 liter), Wright Aeronautical Division R-3350-26WA (Cyclone 18 836C18CA1) twin-row 18-cylinder radial engine, with water/alcohol injection. This engine has a compression ratio of 6.71:1. The R-3350-26W has a Normal Power rating of  2,300 horsepower at 2,600 r.p.m., and a Takeoff/Military Power rating of 2,700 horsepower at 2,900 r.p.m., using 115/145 aviation gasoline. The engine drives a four-bladed Aeroproducts constant-speed propeller with a diameter of 13 feet, 6 inch (4.115 meters) through a 0.4375:1 gear reduction. The engine is 4 feet, 7.62 inches (1.413 meters) in diameter and 6 feet, 6.81 inches (2.002 meters) long. It weighs 2,848 pounds (1,292 kilograms), dry.

The AD-6/A-1H Skyraider had a cruise speed of 198 miles per hour (319 kilometers per hour) and a maximum speed of 322 miles per hour (518 kilometers per hour). The ceiling was 29,400 feet (8,961 meters) and its combat radius carrying 2,000 pounds (907 kilograms) of ordnance was 275 miles (443 kilometers).

A U.S. Marine Corps Douglas AD-2 Skyraider of VMF-121 parked at airfield K-6, Pyongtaek, South Korea, 1952. The hard points under the wings are fully loaded with bombs.
A U.S. Marine Corps Douglas AD-4 Skyraider, Bu. No. 127874, of VMF-121 is parked at airfield K-6, Pyongtaek, South Korea, 1952. The hard points under the wings are fully loaded with bombs. The aircraft is painted overall glossy sea blue. (Navy Pilot Overseas)
Douglas AH-1H Skyraider 52-137593 (U.S. Air Force)
Douglas AH-1H Skyraider 52-137593 of the 602nd Special Operations Squadron. (U.S. Air Force)

The AD-6 Skyraider was armed with four 20mm AN-M2 autocannons, with two in each wing, and 200 rounds of ammunition per gun. The guns fired explosive projectiles with a muzzle velocity of 2,850 feet per second (869 meters per second), and had a rate of fire of 600–700 rounds per minute. The AD-6 could carry 8,000 pounds (3,629 kilograms) of bombs, rockets, gun pods and external fuel tanks from the 15 hard points and pylons under the wings and fuselage.

A Douglas A-1H Skyraider of the 6th Special Operations Squadron dive bombing a target during a close air support mission, Vietnam, 1968. (U.S. Air Force)
A Douglas A-1J Skyraider, 52-142016, of the 6th Special Operations Squadron, dive bombing a target during a close air support mission, Vietnam, 1968. (U.S. Air Force)

Many United States Navy and Marine Corps Skyraiders were transferred to the U.S. Air Force. The Air Force retained the Navy’s Bureau of Aeronautics serial numbers (“Bu. No.”) but added two digits corresponding to the fiscal year in which each airplane was originally contracted. This resulted in serial numbers similar, though longer, than customary in the Air Force and Army numbering system.

The oldest Skyraider in existence is XBT2D-1 Bu. No. 9102. Formerly on display at NAS Oceana, Virginia Beach, Virginia, the airplane was transferred to The Intrepid Sea, Air & Space Museum in New York City for restoration and preservation.

This is the Douglas A-1H Skyraider flown by LCOL Jones, 1 September 1968. Though it was extensively damaged by anti-aircraft gunfire and the subsequent fire, 52-139738 was repaired and returned to service. On 22 September 1972, -738 was shot down over Laos. It was the last Skyraider shot down during the Vietnam War.
Douglas A-1H Skyraider 52-139738, 1st Special Operations Squadron. Lieutenant Colonel William A. Jones III, commanding the 602nd Special Operations Squadron, flew this airplane on 1 September 1968 during a Combat Search and Rescue mission for which he was awarded the Medal of Honor. On 22 September 1972, -738 was shot down over Laos. It was the last Skyraider shot down during the Vietnam War. (U.S. Air Force)

LaVerne Ward Browne was born at Orange, California, 9 December 1906. He was the third child of Edwin J. Brown, a farm worker, and Phebe Alice Proctor Brown. He studied law at the University of Southern California (USC).

“Mystery Plane” poster. (Monogram Pictures Corporation)

In 1928, Brown learned to fly at the Hancock College of Aeronautics, Santa Maria, California. He then worked as a pilot for Transcontinental and Western Airways, flying the Douglas DC-2. He was also commissioned as a second lieutenant in the United States Army Air Corps Reserve.

Browne married Miss Dorothy Leonore Bach at Los Angeles, California, 28 January 1926. They had a daughter, Barbara May Browne, born 6 December 1926, but later divorced. One 12 June 1933, Browne married Harriette Fitzgerald Dodson at Norfolk, Virginia.

From 1931 to 1941, under the pseudonym “John Trent,” Browne performed in sixteen Hollywood movies, including “I Wanted Wings,” with William Holden, Ray Milland and Veronica Lake. He played the character “Tailspin Tommy Tompkins” in four: “Danger Flight,” “Sky Patrol,” “Stunt Pilot,” and “Mystery Plane.”

Browne worked for Douglas Aircraft Company from 1942 to 1957. He died 12 May 1966 at Palos Verdes, California, at the age of 59 years.

“John Trent” (LaVerne Ward Browne) portrayed “Tailspin Tommy Tompkins” in four Hollywood movies. (Monogram Pictures Corporation via IMDb)

© 2017, Bryan R. Swopes

Medal of Honor, First Lieutenant Jack Warren Mathis, United States Army Air Forces

Lieutenant Jack W. Mathis, Air Corps, United States Army. (American Air Museum in Britain UPL-22691)

MEDAL OF HONOR

FIRST LIEUTENANT JACK WARREN MATHIS

Rank and organization: First Lieutenant, U.S. Army Air Corps, 359th Bomb Squadron, 303d Bomb Group.

Place and date: Over Vegesack, Germany, March 18, 1943.

Entered service at: San Angelo, Tex. Born: September 25, 1921, San Angelo, Tex.

G.O. No.: 38, July 12, 1943.

Citation:

The President of the United States of America, in the name of Congress, takes pride in presenting the Medal of Honor (Posthumously) to First Lieutenant (Air Corps) Jack Warren Mathis (ASN: 0-727110), United States Army Air Forces, for conspicuous gallantry and intrepidity above and beyond the call of duty in action with the enemy over Vegesack, Germany, on 18 March 1943, while serving with the 359th Bombardment Squadron, 303d Bombardment Group (H), Eighth Air Force. First Lieutenant Mathis, as leading bombardier of his squadron, flying through intense and accurate anti-aircraft fire, was just starting his bomb run, upon which the entire squadron depended for accurate bombing, when he was hit by the enemy anti-aircraft fire. His right arm was shattered above the elbow, a large wound was torn in his side and abdomen, and he was knocked from his bomb sight to the rear of the bombardier’s compartment. Realizing that the success of the mission depended upon him, First Lieutenant Mathis, by sheer determination and willpower, though mortally wounded, dragged himself back to his sights, released his bombs, then died at his post of duty. As the result of this action the airplanes of his bombardment squadron placed their bombs directly upon the assigned target for a perfect attack against the enemy. First Lieutenant Mathis’ undaunted bravery has been a great inspiration to the officers and men of his unit.

The Medal of Honor and Purple Heart awarded to 1st. Lt. Jack W. Mathis are displayed at the National Museum of the United States Air Force.

Jack Warren Mathis was born 10:30 p.m., 25 September 1921, at San Angelo, Texas. He was the second of three children of Rhude Mark Mathis, a salesman, and Avis Cannon Mathis.

Mathis enlisted as a private in the United States Army, 12 June 1940, at Fort Sam Houston, San Antonio, Texas, and was assigned to the 1st Field Artillery at Fort Sill, Oklahoma. After six months service, he was transferred to the Air Corps as an aviation cadet and sent to Goodfellow Field, southeast of his hometown of San Angelo. He trained as a bombardier, as did his older brother, Rhude Mark Mathis, Jr.

Jack Mathis was commissioned as a second lieutenant on 4 July 1942. He deployed to Europe in September 1942. Mathis was promoted to first lieutenant in January 1943.

Capt. Harold L. Stouse’s combat crew, June 1942. 2nd Lt. Jack W. Mathis is in the back row, far right. (U.S. Air Force)

Lieutenant Mathis was assigned to the combat crew of a Boeing B-17F-25-BO Flying Fortress, 41-24561, of the 359th Bombardment Squadron (Heavy), 303d Bombardment Group (Heavy) at RAF Molesworth. The ship, named The Duchess, was under the command of Captain Harold L. Stouse. It carried fuselage identification markings BN T.

Boeing B-17F-25-BO Flying Fortress 41-24561, The Duchess. Left to right, lower, Sgt. Clyde L. Dewald and Sgt James C. Hicks. Upper, Cpl. Charles H. Stoner. (Roger Freeman Collection, American Air Museum in Britain FRE4205)

Because of the severe effect that German submarines were having against transatlantic merchant convoys, U-boat pens and construction yards were a high-priority target for bombers of the 8th Air Force.

On 18 March 1943, the 8th launched Mission No. 24 against the Bremer-Vulkan-Vegesacker Werft submarine construction yard on the River Weser at Bremen-Vegesack, Germany. The attack force consisted of 76 B-17s and 27 B-24 Liberators. Each bomber was loaded with six 1,000 pound (454 kilogram) M44 high-explosive bombs. The plan called for bombers to drop from 24,000 feet (7,315 meters). Each squadron would release their bombs simultaneously.

Mission No. 24 was Jack Mathis’ fourteenth combat mission. He was the lead bombardier of the 359th, the second element of seven B-17s of the 303d Group. The bombardier controlled the heading of the B-17 through adjustments to his Norden bomb sight. The squadron’s bombing accuracy was dependent on the skill of the lead bombardier.

The B-17F at the bottom of the image is The Duchess, 41-24561. (Roger Freeman Collection, American Air Museum in Britain, FRE 4264)

As the American bombers approached the target, Mathis took careful aim at the target 24,000 feet below and opened the bomb bay doors. With his eye pressed to the Norden bombsight, Mathis was less than one minute away from releasing his bombs when an antiaircraft shell exploded near the right nose of his B-17, named The Duchess. Fragments from the shell shattered the Plexiglas nose, nearly severed his right arm above the elbow, and caused deep wounds in his side and abdomen. The concussion threw him to the rear of the nose section. Nevertheless, Mathis went back to his bombsight and accurately dropped his bombs before collapsing dead over his bombsight.

—Excerpted from A Test of Courage: 1st Lt. Jack W. Mathis, an article from the National Museum of the United States Air Force, 1 May 2015

Reconnaissance photographs later revealed that seven enemy submarines and two-thirds of the shipyard had been destroyed in the attack. For his extraordinary effort, 1st Lt. Jack W. Mathis posthumously received the Medal of Honor, the first awarded to an 8th Air Force Airman.

Boeing B-17 Flying Fortress heavy bombers leave contrails at high altitude. (United States Air Force)

Jack Mathis’ older brother, Lieutenant Rhude Mark Mathis, Jr., was at RAF Molesworth awaiting his brother’s return from the mission. He was present when The Duchess landed. Mark Mathis requested a transfer to the Captain Stouse’s crew with 359th to take his brother’s place. Tragically, on his fourth mission, he, too, was killed.

First Lieutenant Jack Warren Mathis was buried at Fairmount Cemetery, San Angelo, Texas. His brother, First Lieutenant Rhude Mark Mathis, Jr., is buried at the Netherlands American Cemetery and Memorial, Margraten, Netherlands.

Mathis Field (San Angelo Regional Airport, or SJT) was named after the two Mathis brothers.

Lieutenant Jack W. Mathis’ Medal of Honor is displayed at the National Museum of the United States Air Force, Wright Patterson Air Force Base, Ohio.

The Duchess survived 59 combat missions. It was returned to the United States after the war in Europe came to an end. The bomber was scrapped in August 1945.

Boeing B-17F Flying Fortress

© 2021 Bryan R. Swopes