Tag Archives: Wright Aeronautical Division

5 April 1950

Martin JRM-3 Mars Bu. No. 76822, Marshall Mars, burning off Diamond Head, Oahu, Hawaiian Islands, 5 April 1950. (U.S. Navy)
Martin JRM-3 Mars Bu. No. 76822, Marshall Mars, burning off Diamond Head, Oahu, Hawaiian Islands, 5 April 1950. (U.S. Navy)

While on a test flight following an engine change, a United States Navy Martin JRM-3 Mars seaplane, Marshall Mars, Bu. No. 76822, suffered an engine fire (inboard, left wing) and made an emergency landing at Ke’ehi Lagoon, off Diamond Head, Hawaii, 5 April 1950. The airplane’s crew was rescued but the airplane exploded and sank.

The wreck was discovered on the sea floor in August 2004 at a depth of approximately 1,400 feet (427 meters).

The Martin JRM Mars was a large four-engine flying boat transport built by the Glenn L. Martin Company for the U. S. Navy. originally designed as a patrol bomber, the prototype XPB2M-1 Mars made its first flight on 3 July 1942, Only five transport variants were built, four designated JRM-1, with the last one being a JRM-2. Each airplane was given an individual name derived from the names of island chains in the Pacific Ocean: Marianas MarsHawaii MarsPhilippine MarsMarshall Mars and Caroline Mars. These airplanes were used to transport personnel and cargo between the West Coast of the United States and the Hawaiian Islands. All were upgraded to JRM-3.

Four Martin JRM-3 Mars flying boats in formation. (U.S. Navy)
Four Martin JRM-3 Mars flying boats in formation. (U.S. Navy)

The Martin JRM-2 Mars had a normal crew of 4, with accommodations for a relief crew. It was designed to carry 138 combat troops or 34,000 pounds (15,422 kilograms) of cargo. It was 120 feet, 3 inches (36.652 meters) long with a wingspan of 200 feet, 0 inches (60.960 meters) and height of 43 feet, 8 inches (13.310 meters), with beaching gear. The wing area was 3,686 square feet (342.4 square meters). The flying boat had an empty weight of 80,701 pounds (36,605 kilograms) and a maximum takeoff weight (MTOW) 0f 165,000 pounds (74,843 kilograms).

Martin JRM-2 Mars three-view illustration with dimensions. (U.S. Navy)

A NASA publication states, “A zero-lift drag coefficient of 0.0233 and a maximum lift-drag ratio of 16.4 made the JRM the most aerodynamically efficient of any of the flying boats. . . .”

Martin JRM-3 Mars, Bu.No. 76822, Marshall Mars. (U.S. Navy)
Martin JRM-3 Mars, Bu.No. 76822, Marshall Mars. (U.S. Navy)

The Martin Mars was powered by four air-cooled, supercharged, direct-fuel-injected, 3,347.662-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division R-3350-24WA (Cyclone 18 825C18BD1) (also known as the Duplex-Cyclone), a two-row 18-cylinder radial engines with a compression ratio of 6.70:1 and water/alcohol injection. This engine has a normal power rating of 2,000 horsepower at 2,400 r.p.m at 5,500 feet (1,676 meters) and 1,800 horsepower at 2,400 r.p.m. at 15,000 feet (4,572 meters). The engine’s takeoff power rating is 2,500 horsepower at 2,900 r.p.m. 100/130 octane aviation gasoline was required. The engines drove four-bladed 16 foot, 8 inch (5.080 meter) Curtiss Electric variable-pitch propellers through a 0.4375:1 gear reduction. (After modification to the JRM-3, the propellers on the inboard engines were reversible.) The R-3350-24WA is 6 feet, 8.58 inches (2.047 meters) long, and 4 feet, 6.13 inches (1.375 meters) in diameter. Its dry weight is 2,822 pounds (1,280 kilograms).

The JRM-3 had a cruise speed of 165 knots (190 miles per hour/306 kilometers per hour) and a maximum speed of 211 knots (243 miles per hour/391 kilometers per hour) at 15,600 feet (4,755 meters). The service ceiling was 19,700 feet (6,005 meters) and its range was 3,790 nautical miles (4,361 statute miles/7,019 kilometers).

A U.S. Navy Martin JRM Mars. (Glenn L. Martin Co.)
A U.S. Navy Martin JRM Mars. (Glenn L. Martin Co.)

© 2019, Bryan R. Swopes

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4–15 March 1957

U.S. Navy ZPG-2 Bu. No. 141561, “Snow Bird,” prior to departure at NAS South Weymouth, Boston, Massachusetts, 4 March 1957 (NASM)

4 March 1957: At 6:30 p.m., Eastern Standard Time, a United States Navy non-rigid airship, Goodyear ZPG-2, Bu. No. 141561, departed NAS South Weymouth, Boston, Massachussetts, on a long-dstance flight to demonstrate the capabilities of a modern lighter-than-air military “blimp.” The airship had been involved in cold-weather testing and had been given the name, Snow Bird. During this flight, the blimp used the radio call sign “Planner 12.”

CDR Jack R. Hunt, USNR, briefs the crew of Snow Bird prior to departure, 4 March 1957. (Flying Magazine)

Snow Bird was under the command of Commander Jack Reed Hunt, U.S.N.R., a fifteen-year veteran of airship operations. There were two additional pilots, Commander Ronald W. Hoel, U.S.N., and Lieutenant Commander Robert S. Bowser, U.S.N. The crew also consisted of three navigators, Lieutenant Stanley W. Dunton, Lieutenant Charles J. Eadie, and Lieutenant John R. Fitzpatrick. The remainder of the crew were Chief Aviation Electronicsman (ALC) Lee N. Steffan, crew chief and radio; Aviation Machinist’s Mate 1st Class (AD1) Thomas L. Cox, flight mechanic; Aviation Electricians’s Mate 1st Class (AE1) Carl W. Meyer, electrician; Aerographer’s Mate 1st Class (AG1) William S.Dehn, Jr., aerologist and photographer; Aviation Machinist’s Mate 2nd Class (AD2) James R. Burkett, Jr., flight mechanic; Aviation Metalsmith 2nd Class (AM2) George A. Locklear, rigger and cook; and Aviation Electrician’s Mate 2nd Class (AT2) Frank J. Maxymillian, radio. Also on board the air ship was a civilian flight engineer, Mr. Edgar L Moore, a Goodyear Aircraft Corporation Field Representative.

Goodyear ZPG-2. (U.S. Navy)

Snow Bird headed east across the Atlantic Ocean, passing north of the Azores on 7 March. At this point, the airship had burned off enough fuel that it was light enough to cruise on one engine. This allowed a much greater range. (A lateral rive shaft between engines allowed both propellers to continue turning.) Late in the third day the flight, the blimp reached the west coast of Portugal, having completed the first Atlantic crossing by a lighter-than-air craft in 12 years.

Snow Bird turned south, heading for Casablanca on the west coast of North Africa, which it reached the morning of 8 March. The airship continued south along the African coast before turning west to re-cross the ocean. The route took the blimp past the Canary and Cape Verde Islands, and then onward to the Virgin Islands. Arriving back in the United States, Snow Bird made landfall at Miami Beach on the afternoon of 14 March.

Admiral Arleigh Burke

A radio message was sent to the crew of Planner 12 by Admiral Arleigh Burke, Chief of Naval Operations:

HEARTIEST CONGRATULATIONS ON ESTABLISHING A NEW WORLD ENDURANCE RECORD FOR AIRSHIPS X YOUR UNTIRING EFFORTS AND DEVOTION ARE MOST COMMENDABLE X THIS FLIGHT DEMONSTRATES AN INCREASED ASW AND AEW CAPABILITY AND OTHER ACHIEVEMENTS WHICH SERVE TO DEMONSTRATE A CONTINUING SEARCH FOR TECHNOLOGICAL ADVANCES BY THE U S NAVY X WELL DONE X ARLEIGH BURKE

Not finished with its voyage, the airship next headed to Dry Tortugas at the far western end of the Florida Keys, and then finally landed at NAS Key West, Florida, on 15 March.

ZPG-2 Flight Track (Flying Magazine)

Snow Bird had traveled 9,448 miles (15,205 kilometers) without landing or refueling. The Fédération Aéronautique Internationale (FAI) lists this as “the longest recorded airship flight.” This exceeded the distance record set by Graf Zeppelin, flying from Friedrichshaven, Germany, to Tokyo, Japan, (11,247 kilometers) 15–19 August 1929. From takeoff at NAS South Weymouth to landing at NAS Key West, the total duration of the flight was 264 hours, 14 minutes.

The crew was met by a large group of dignitaries. Commander Reed was presented the Distinguished Flying Cross by Fleet Admiral William Frederick Halsey, Jr., United States Navy, one of the greatest military leaders of World War II.

Commander Hunt was later presented the Harmon International  Trophy by President Dwight D. Eisenhower.

An AEW variant U.S. Navy Goodyear ZPG airship. (The Noon Balloon)

Goodyear ZPG-2 Bu. No. 141561 was built by the Goodyear Aircraft Corporation at Akron, Ohio. It was the 11th of 12 “N-class” airships which were used for patrol, anti-submarine warfare ASW), and when equipped with radar, for airborne early warning (AEW).

The ZPG-2 is 343 feet (105 meters) long and the envelope has a maximum diameter of 76 feet (23 meters). A two-deck control car was suspended beneath the envelope. The airship had an overall height of 107 feet (33 meters). Bouyancy was provided by 1,011,000 cubic feet (28,628 cubic meters) of Helium.

There are four fins placed in a X-pattern at the tail of the ZPG-2, called ruddervators. (These were similar to the fins used on the experimental submarine USS Albacore (AGSS-569) several years later.) The ruddervators allowed the airship to be controlled by a single control column, a change from the two controls used previously. Also, the decreased vertical span of the fins allowed greater ground clearance, so that the blimp could takeoff at steeper angles than if it had been equipped with the standard cruciform fins.

N-class blimp N-1. Compare its fins to those of the airship in the background.

The Goodyear ZPG-2 was powered by two air-cooled, supercharged, 1,301.868 cubic inch displacement (21.334 liter) Wright Aeronautical Division R-1300-2 (Cyclone 7 865C7BA1) seven-cylinder radial engines mounted outside the control car. The R-1300-2 was a direct-drive engine with a compression ratio of 6.2:1. It was rated at 700 horsepower at 2,400 r.p.m., and 800 horsepower at 2,600 r.p.m., for takeoff, using 91/96 octane aviation gasoline. The engines turned three-bladed Curtiss Electric variable pitch, reversible propellers. The R-1300-2 was 48.12 inches (1.222 meters) long, 50.45 inches (1.281 meters) in diameter, and weighed 1,067 pounds (484 kilograms).

The ZPG-2 had a cruise speed of 57 miles per hour (92 kilometers per hour) and maximum speed of 80 miles per hour (129 kilometers per hour). Its normal endurance was three days.

Bu. No. 141561’s cockpit, nose cone and a frame of a ruddervator are displayed at the National Naval Aviation Museum, NAS Pensacola, Florida.

Jack Reed Hunt

Jack Reed Hunt was born at Red Oak, Iowa, 18 May 1918. He was the second of seven children of Smith Reed Hunt, a baker, and Blanche Luise Seefeldt Hunt. The family moved to southern California, where Jack grew up.

Jack R. Hunt joint the United States Navy on 4 April 1942. He was trained as an airship pilot and flight instructor. Hunt was commissioned as an Ensign in the United States Naval Reserve, 1 October 1942, and promoted to Lieutenant (junior grade), 1 October 1943. Hunt remained in the Navy following World War II. He was promoted to Lieutenant Commander 1 August 1951, and to Commander, 1 July 1956.

From 1963 until 1984, Jack Hunt was the president of Embry-Riddle Aeronautical University, a fully-accredited aerospace university.

Hunt was married three times (Bethel, Donna and Lynne) and had seven children. He died 7 January 1984, at the age of 65 years.

© 2019, Bryan R. Swopes

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20 December 1943

Technical Sergeant Forrest Lee Vosler, Air Corps, United States Army. (U.S. Air Force)

MEDAL OF HONOR

VOSLER, FORREST L.

(Air Mission)

          The President of the United States takes pleasure in awarding the MEDAL of HONOR to

STAFF SERGEANT FORREST L. VOSLER,

AIR CORPS, UNITED STATES ARMY,

for service as set forth in the following

CITATION:

         “For conspicuous gallantry in action against the enemy above and beyond the call of duty while serving as a radio operator-air gunner on a heavy bombardment aircraft in a mission over Bremen, Germany, on 20 December 1943. After bombing the target, the aircraft in which T/Sgt. Vosler was serving was severely damaged by antiaircraft fire, forced out of formation, and immediately subjected to repeated vicious attacks by enemy fighters. Early in the engagement a 20-mm. cannon shell exploded in the radio compartment, painfully wounding T/Sgt. Vosler in the legs and thighs. At about the same time a direct hit on the tail of the ship seriously wounded the tail gunner and rendered the tail guns inoperative. Realizing the great need for firepower in protecting the vulnerable tail of the ship, T/Sgt. Vosler, with grim determination, kept up a steady stream of deadly fire. Shortly thereafter another 20-mm. enemy shell exploded, wounding T/Sgt. Vosler in the chest and about the face. Pieces of metal lodged in both eyes, impairing his vision to such an extent that he could only distinguish blurred shapes. Displaying remarkable tenacity and courage, he kept firing his guns and declined to take first-aid treatment. The radio equipment had been rendered inoperative during the battle, and when the pilot announced that he would have to ditch, although unable to see and working entirely by touch, T/Sgt. Vosler finally got the set operating and sent out distress signals despite several lapses into unconsciousness. When the ship ditched, T/Sgt. Vosler managed to get out on the wing by himself and hold the wounded tail gunner from slipping off until the other crewmembers could help them into the dinghy. T/Sgt. Vosler’s actions on this occasion were an inspiration to all serving with him. The extraordinary courage, coolness, and skill he displayed in the face of great odds, when handicapped by injuries that would have incapacitated the average crew member, were outstanding.”

/s/ Franklin D. Roosevelt

Technical Sergeant Forrest L. Vosler, United States Army Air Corps, is awarded the Medal of Honor by President Franklin Delano Roosevelt in a ceremony in the Oval Office of the White House, Washington, D.C. (U.S. Air Force)
Technical Sergeant Forrest L. Vosler, Air Corps, United States Army, is awarded the Medal of Honor by President Franklin Delano Roosevelt in a ceremony in the Oval Office of the White House, Washington, D.C., 31 August 1944. Shaking Sergeant Vosler’s hand is Under Secretary of War Robert Porter Patterson, Sr. (U.S. Air Force)

Staff Sergeant Forrest Lee Vosler was the radio operator/top gunner aboard the Boeing B-17F-65-BO Flying Fortress 42-29664, Jersey Bounce, Jr.,¹ one of 21 B-17s of the 303rd Bombardment Group, Heavy, sent on Mission No. 90, an attack against Bremen, Germany. The bomber was under the command of 2nd Lieutenant John F. Henderson. Captain Merle R. Hungerford, an instructor pilot, acted as co-pilot. The bombers encountered heavy antiaircraft fire over the target, and were attacked by as many as 125 enemy fighters. Bombing from an altitude of  26,200 feet (7,986 meters), the B-17s dropped 24 tons of incendiary bombs.

Staff Sergeant Forrest Lee Volser was the radio operator on this Boeing B-17F-65-BO Flying Fortress, 42-29664, the “Jersey Bounce Jr.” (U.S. Air Force)

Jersey Bounce, Jr. was hit by anti-aircraft artillery just after its bomb load was released. The number 1 engine, outboard, left wing, and the number 4 engine, outboard, right wing, were damaged. When the B-17 slowed and dropped out of its formation, it became a target of opportunity for the Luftwaffe fighters.

The crew reported that as many as ten fighters attacked, one after another. Flight engineer and top turret gunner Staff Sergeant William H. Simpkins, Jr., was credited with destroying a Focke-Wulf Fw 190 fighter, and right waist gunner Sergeant Ralph F. Burkart shot down a Messerschmitt Me 210 twin-engine heavy fighter. Sergeant Stanley E. Moody, the left waist gunner, destroyed a Messerschmitt Bf 109 and probably shot down a Messerschmitt Bf 110 twin-engine fighter.

The heavily-damaged bomber flew at low altitude as it headed for the North Sea, and then toward England. Vosler sent repeated distress signals which allowed search and rescue aircraft to locate the B-17. Lieutenant Henderson ditched 42-29644 within sight of land. The crew were quickly rescued by a small coastal freighter, MV Empire Sportsman.² The bomber crew was then transferred to a British air-sea rescue boat.

Forrest Lee Vosler was born at Lyndonville, New York, 29 July 1923. He was the son of William I. Vosler, a farmer, and Lottie I. Furness Volser. He attended Livonia Central High School, Livonia, New York, graduating in 1941. He was employed as a drill press operator by General Motors at Rochester, New York.

Forrest Lee Vosler enlisted in the Air Corps, United States Army, at Rochester, 8 October 1942. He was 6 feet, 1 inch (1.854 meters) tall and weighed 147 pounds (66.7 kilograms). After completing basic training at Atlantic City, New Jersey, Private Vosler trained as a radio operator at Scott Field, Illinois, and as an aerial gunner at Harlingen, Texas. After completing training Private Vosler was promoted to Sergeant, 25 May 1943. In August 1943, he was promoted to Staff Sergeant. Deployed to the United Kingdom, Staff Sergeant Vosler was assigned to the 358th Bombardment Squadron, Heavy, of the 303rd Bombardment Group, Heavy, at RAF Molesworth (AAF-107), Cambridgeshire, England.

Technical Sergeant Vosler was the third of only four enlisted airmen two be awarded the Medal of Honor during World War II. Vosler was hospitalized for the next 12 months. After recuperating from his wounds, Vosler was discharged from the Army Air Corps, 17 October 1944. In addition to the Medal of Honor, Forrest Vosler had been awarded the Silver Star, the Purple Heart, Air Medal, Army Good Conduct Medal, American Campaign Medal, European-African-Middle Eastern Campaign Medal with one bronze service star, World War II Victory Medal and the Presidential Unit Citation.

Following the War, Forrest Volser was employed as an engineer at radio station WSYR, the oldest continuously operating radio station in the Syracuse, New York, area. He attended the College of Business Administration, Syracuse University, at Syracuse, New York. He was a member of the Sigma Chi (ΣΧ) fraternity.

Forrest Vosler married Miss Virginia Frances Slack, 28 October 1945, at the Grace Episcopal Church, Syracuse, New York. The ceremony was presided over by Rev. James R. Rockwell. They would have a daughter, Sondra Lee Vosler, and a son, Marcellus Vosler.

Vosler had lost one eye and found that blurred vision in his remaining eye made it impossible to keep up with his studies. He dropped out of college at the end of the 1945 fall semester.

“Woody” Vosler worked for the Veterans Administration for thirty years.

Forrest Lee Vosler died at Titusville, Florida, 17 February 1992 at the age of 68 years. He was buried at Arlington National Cemetery.

The Forrest L. Vosler Noncommissioned Officer Academy and the Forrest L. Vosler Veterans Memorial Park at Peterson Air Force Base, Colorado, are named in his honor.

A Boeing B-17F Flying Fortress (B-17F-95-BO 42-30243). (U.S. Air Force)

Boeing B-17F-65-BO Flying Fortress 42-29664, Jersey Bounce, Jr. The bomber was on its 32nd combat mission. It had been flown by at least nine different pilots and with different combat crews.

42-29664 was delivered from the Boeing plant in Seattle, Washington, to Denver, Colorado, 30 January 1943. It arrived at Salina, Kansas, 12 February 1943, and was sent on to Morrison, New Jersey, 28 February 1943. It was then flown across the north Atlantic Ocean to England. The new B-17F was assigned to the 358th Bombardment Squadron, 303rd Bombardment Group (Heavy), at RAF Molesworth, Cambridgeshire, England, 21 March 1943. It carried group identification markings VK C painted on its fuselage.

The Boeing B-17F Flying Fortress was a four-engine heavy bomber operated by a flight crew of ten. It was 74 feet, 9 inches (22.784 meters) long with a wingspan of 103 feet, 9.375 inches (31.633 meters) and an overall height of 19 feet, 1 inch (5.187 meters). Its empty weight was 34,000 pounds (15,422 kilograms), 40,437 pounds (18,342 kilograms) loaded, and the maximum takeoff weight was 56,500 pounds (25,628 kilograms).

Boeing B-17F Flying Fortress. (U.S. Air Force)

The B-17F was powered by four air-cooled, supercharged, 1,823.129-cubic-inch-displacement (29.875 liters) Wright Cyclone C9GC (R-1820-97) nine-cylinder radial engines with turbochargers, producing 1,200 horsepower at 2,500 r.p.m. for takeoff and 1,000 horsepower at 2,300 r.p.m. at Sea Level. War Emergency Power was 1,380 horsepower. The Cyclones turned three-bladed constant-speed Hamilton-Standard Hydromatic propellers with a diameter of 11 feet, 7 inches (3.835 meters) though a 0.5625:1 gear reduction.  The R-1820-97 engine is 47.80 inches (1.214 meters) long and 55.10 inches (1.399 meters) in diameter. It weighs 1,315 pounds (596 kilograms).

These engines gave the B-17F a cruising speed of 200 miles per hour (322 kilometers per hour). The maximum speed was 299 miles per hour (481 kilometers per hour) at 25,000 feet, though with War Emergency Power, the bomber could reach 325 miles per hour (523 kilometers per hour) at 25,000 feet for short periods. The service ceiling was 37,500 feet (11,430 meters).

With a normal fuel load of 2,520 gallons (9,540 liters) the B-17F had a maximum range of 2,880 miles (4,635 kilometers). Carrying a 6,000 pound (2,722 kilogram) bomb load, the range was 1,300 miles (2,092 kilometers).

358th Bombardment Squadron flight crew. Most of the men in this photograph were aboard "Jersey Bounce Jr.", 20 December 1943. Front, left to right: Sgt. Edward Ruppel. ball turret gunner; T/Sgt. Forest L. Vosler, radio operator; S/Sgt. William H. Simpkins, Jr., flight engineer/top turret gunner; Sgt. Gratz, tail gunner 9replaceing teh critically wounded Sgt. George W. Burke, who was rescued by Vosler); Sgt. Raaplh F. Burkhart, waist gunner. Rear, left to right: 2nd Lt. Warren S. Wiggins, navigator; 2nd Lt. Woodrow W. Monkres, bombardier; 2 Lt. Walter J. Ames, co-pilot; 2nd Lt. John F. Henderson, aircraft commander. (U.S. Air Force)
358th Bombardment Squadron flight crew. Most of the men in this photograph were aboard “Jersey Bounce Jr.”, 20 December 1943. Front, left to right: Sgt. Edward Ruppel, ball turret gunner; T/Sgt. Forest L. Vosler, radio operator/top gunner; S/Sgt. William H. Simpkins, Jr., flight engineer/top turret gunner; Sgt. Gratz, tail gunner (replacing the critically wounded Sgt. George W. Burke, who was rescued by Vosler); Sgt. Ralph F. Burkhart, waist gunner. Rear, left to right: 2nd Lt. Warren S. Wiggins, navigator; 2nd Lt. Woodrow W. Monkres, bombardier; 2 Lt. Walter J. Ames, co-pilot; 2nd Lt. John F. Henderson, aircraft commander. (U.S. Air Force)

The B-17F Flying Fortress was armed with up to 13 air-cooled Browning AN-M2 .50-caliber machine guns. Power turrets mounting two guns each were located at the dorsal and ventral positions.

The maximum bomb load was 20,800 pounds over very short ranges. Normally, 4,000–6,000 pounds (1,815–2,722 kilograms) were carried. The internal bomb bay could be loaded with a maximum of eight 1,600 pound (725.75 kilogram) bombs. Two external bomb racks mounted under the wings between the fuselage and the inboard engines could carry one 4,000 pound (1,814.4 kilogram) bomb, each, though this option was rarely used.

The B-17 Flying Fortress first flew in 1935, and was was in production from 1937 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.) 3,405 of the total were B-17Fs, with 2,000 built by Boeing, 605 by Douglas and 500 by Lockheed-Vega.

Only three B-17F Flying Fortresses remain in existence.

This restored Boeing B-17F-70-BO Flying Fortress, 42-29782, is on display at The Museum of Flight at Seattle's Boeing Field. (Boeing)
This restored Boeing B-17F-70-BO Flying Fortress, 42-29782, is on display at The Museum of Flight at Seattle’s Boeing Field. (Boeing)

¹ “Jersey Bounce” was a popular song of 1942.

² M/V Empire Sportsman was built by Richards Ironworks Ltd., Lowestoft, Suffolk, 1943. 325 Gross Registered Tons.

© 2017, Bryan R. Swopes

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3 November 1950

Mont Blanc, western face. The summit was most recently measured at 4,810.06meters. 18 meters of snow and ice cover the actual rock peak, at 4,792 meters.
Mont Blanc, western face. The summit was most recently measured at 4,810.06 meters (15,781.04 feet). 18 meters (59 feet) of snow and ice cover the actual rock peak, at 4,792 meters.

3 November 1950: Air India Flight 245, a Lockheed L-749A Constellation, VT-CQP, Malabar Princess, was on a flight from Bombay, India, to London, England, with intermediate stops at Cairo, Egypt and Geneva, Switzerland. The aircraft was under the command of Captain Alan R. Saint, with co-pilot Vijay Yeshwant Korgaokar, three navigators and a radio operator.

Air India’s Lockheed L-749A Constellation, VT-CQP, Malabar Princess. (ETH Zurich)

At 9:43 a.m., Malabar Princess crashed into the Rochers de la Tournette (Tournette Spur) on the west side of Mont Blanc at an approximate elevation of 15,344 feet (4,677 meters). All 48 persons on board were killed.

Air India International was the national airline of India, having been formed from Tata Airlines. On 8 June 1948, Air India’s first scheduled flight departed Bombay for Cairo, Geneva and London. The airliner was Malabar Princess.

On 24 January 1966, Air India Flight 101, a Boeing 707-437, VT-DMN, named Kanchenjunga,¹ crashed at almost the same location on Mount Blanc. All 117 persons on board were killed.

The Lockheed L-749A Constellation was operated by a flight crew of four, with two to four flight attendants. It could carry up to 81 passengers. The airplane was 97 feet, 4 inches (29.667 meters) long with a wingspan of 123 feet (37.490 meters) and an overall height of 22 feet, 5 inches (6.833 meters). It had an empty weight of 56,590 pounds (25,669 kilograms) and maximum takeoff weight of 107,000 pounds (48,534 kilograms).

The L-749A was powered by four air-cooled, supercharged and fuel-injected 3,347.66-cubic-inch-displacement (54.858 liter) Wright Aeronautical Division Cyclone 18 (also known as the Duplex-Cyclone) 749C18BD1 two-row 18-cylinder radial engines with a compression ratio of 6.5:1. They had a Normal Power rating of 2,100 horsepower at 2,400 r.p.m., and Takeoff Power rating 2,500 horsepower at 2,800 r.p.m. (five minute limit). The engines drove three-bladed Curtiss-Electric propellers through a 0.4375:1 gear reduction. This engine featured “jet stacks” which converted the piston engines’ exhaust to usable jet thrust, adding about 15 miles per hour (24 kilometers per hour) to the airplane’s speed. The 749C18BD1 was  6 feet, 6.52 inches (1.994 meters) long, 4 feet, 7.62 inches (1.413 meters) in diameter, and weighed 2,915 pounds (1,322 kilograms).

The L-749 had a cruise speed of 345 miles per hour (555 kilometers per hour) and a range of 4,995 miles (8,039 kilometers). Its service ceiling was 24,100 feet (7,346 meters).

A sister ship of Malabar Princess, this is Air India's Lockheed L-749A Constellation VT-CQS. (Lockheed via R.A. Schofield. Photograph used with permission.)
A sister ship of Malabar Princess, this is Air India’s Lockheed L-749A Constellation VT-CQS. (Lockheed via R.A. Schofield. Photograph used with permission.)

The Air India Flight 245 crash was the basis for a novel, La neige en deuil (“The Snow in Mourning”), written by Henri Troyat (née Lev Aslanovic Tarassov), which in turn inspired the 1956 Edward Dymtryk motion picture, “The Mountain.” The film starred Spencer Tracy, Robert Wagner and Anna Kashfi.² Tracy was nominated by the British Academy of Film and Television Arts for an award for his performance.

The great American actor Spencer Tracy starred as a mountain guide in Edward Dmytryk's 1956 motion picture, "The Mountain." (Paramount)
The great American actor Spencer Tracy starred as Alpine mountain guide “Zachary Teller” in Edward Dmytryk’s 1956 motion picture, “The Mountain.” (Paramount)

¹ Kanchenjunga is the name of the world’s third highest mountain, an “eight thousander” located 125 kilometers (78 miles) east-southeast of Mount Everest in the Himalayas. Its summit is 8,598 meters (28,209 feet) above Sea Level. It is considered to be a sacred mountain. Climbers are not allowed there.

² Anna Kashfi (née Joan O’Callaghan) was the first Mrs. Marlon Brando.

© 2018, Bryan R. Swopes

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5 October 1954

Lockheed XF-104 Starfighter 083-1002, serial number 53-7787, the second prototype, in flight near Edwards AFB. (U.S. Air Force)

5 October 1954: Chief Engineering Test Pilot Tony LeVier made the first flight in the second prototype Lockheed XF-104 Starfighter, 53-7787, at Edwards Air Force Base in the high desert of southern California. This was the armament test aircraft and was equipped with a General Electric T171 Vulcan 20mm Gatling gun. This six-barreled gun was capable of firing at a rate of 6,000 rounds per minute.

The XF-104 was 49 feet, 2 inches (14.986 meters) long with a wingspan of 21 feet, 11 inches (6.680 meters) and overall height of 13 feet, 6 inches (4.115 meters). The prototypes had an empty weight of 11,500 pounds (5,216 kilograms) and maximum takeoff weight of 15,700 pounds (7,121 kilograms).

While the first prototype, 53-7776, was equipped with a Buick J65-B-3 turbojet engine, the second used a Wright Aeronautical Division J65-W-6 with afterburner. Both were improved derivatives of the Armstrong Siddely Sa.6 Sapphire, built under license. The J65 was a single-shaft axial-flow turbojet with a 13-stage compressor and 2-stage turbine. The J65-B-3 was rated at 7,330 pounds of thrust, and the J65-W-6, rated at 7,800 pounds (34.70 kilonewtons), and 10,500 pounds (46.71 kilonewtons) with afterburner.

The XF-104 had a maximum speed of 1,324 miles per hour (2,131 kilometers per hour), a range of 800 miles (1,287 kilometers) and a service ceiling of 50,500 feet (15,392 meters).

53-7787 was lost 19 April 1955 when it suffered explosive decompression at 47,000 feet (14,326 meters) during a test of the T171 Vulcan gun system. The lower escape hatch had come loose due to an inadequate latching mechanism. Lockheed test pilot Herman R. (“Fish”) Salmon was unable to find a suitable landing area and ejected at 250 knots (288 miles per hour/463 kilometers per hour) and 15,000 feet (4,572 meters). The XF-104 crashed 72 miles (117 kilometers) east-northeast of Edwards Air Force Base. Salmon was found two hours later, uninjured, about 2 miles (3.2 kilometers) from the crash site.

Tony LeVier with the XF-104 armament test prototype, 53-7787, at Edwards AFB, 1954. LeVier is wearing a David Clark Co. T-1 capstan-type partial-pressure suit with K-1 helmet. (U.S. Air Force)

The YF-104A pre-production aircraft and subsequent F-104A production aircraft had many improvements over the two XF-104 prototypes. The fuselage was lengthened 5 feet, 6 inches (1.68 meters). The J65 engine was replaced with a more powerful General Electric J79-GE-3 turbojet. There were fixed inlet cones added to control airflow into the engines. A ventral fin was added to improve stability.

Lockheed F-104A-15-LO Starfighters 56-0769 and 56-0781. (Lockheed Martin)

© 2019, Bryan R. Swopes

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