12 December 1947

Boeing XB-47 Stratojet rollout at Seattle, Washington, 12 December 1947. (U.S. Air Force 061024-F-1234S-065)

12 December 1947: The Boeing XB-47 Stratojet was rolled out of its hangar for public display.

The Arizona Republic reported:

Boeing’s New Jet Bomber Is The Size of Superfort

     SEATTLE, Sept. 13—(AP) A new jet-propelled bomber, the size of a B-29 Superfortress and with sharply sweptback wings and tail surfaces will begin ground and taxiing tests soon.

     Whether the new Boeing XB-47 Stratojet, rolled out of its construction hangar for the first public display yesterday will near or attain speeds of jet fighter planes remains undisclosed. The army air forces and Boeing, showing the plane, made no mention of its expected speed, but streamlining was carried to the extreme.

     The sharply turned-back or inverted wings and tail surfaces appeared to be notable innovations in plane design. Four general Electric-built jet engines are mounted in pairs under the inboard sections of the wing, with another out near each wing tip.

     The wings are also “exceptionally thin,” a Boeing spokesman said, and the plane has a tandem type landing gear with small outrigger wheels. What was also described as 18 jet-assisted takeoff units studded the rear fuselage for added power. There was only one bomb bay, compared with the two on a B-29, but it was longer than those on a Superfortress.

     Compared with the B-29’s wing span of 141 feet and length of 99 feet, the XB-47’s wing span is approximately 116 feet and its length about 108 feet.

     Robert Robbins and Scott Osler, chosen as the plane’s test pilots a year ago, said it would be probably a month or more before it could take to the air. They said its initial flights would be “admittedly hazardous” but believe it will be an “outstanding airplane.”

     Blueprints used in planning the ship provides for two rocket motors near the tail, to be used for emergency bursts of power, experts said. It would be the first combat-type aircraft with such equipment.

     The Boeing company has turned out three other new-type planes this year. They were the new B-50, the successor to the Superfortress, the first 80-passenger Stratocruiser and the XL-15 Liaison plane, being built at the Wichita, Kan., plant.

     Several other jet bombers are under experiment for the army and the Consolidated Vultee XB-46, powered with four engine, and the North American XB-45, also a four-engine plane, have undergone trial flights.

The Arizona Republic, Vol. 58, No. 116, 14 September 1947, Page 12, Columns 1–3

Boeing XB-47 Stratojet 46-065. (U.S. Air Force 061024-F-1234S-004)

The first prototype, 46-065, was powered by six General Electric J35-GE-7 axial flow turbojet engines in four pods mounted on pylons below the wings. The J35 was a single-spool, axial-flow turbojet engine with an 11-stage compressor and single-stage turbine. The J35-GE-7 was rated at 3,750 pounds of thrust (16.68 kilonewtons) at 7,700 r.p.m. (static thrust, Sea Level). The engine was 14 feet, 0.0 inches (4.267 meters) long, 3 feet, 4.0 inches (1.016 meters) in diameter and weighed 2,400 pounds (1,089 kilograms). (The second prototype, 46-066, was completed with J47 engines. 46-065 was later retrofitted with these engines.)

The XB-47 prototype had a maximum speed of 502 knots (578 miles per hour/930 kilometers per hour/0.80 Mach) at 15,000 feet (4,572 meters). The combat speed was 462 knots (532 miles per hour/856 kilometers per hour/0.70 Mach) at 35,000 feet (10,668 meters). The prototype’s empty weight was 74,623 pounds (33,848 kilograms), while its maximum takeoff weight was 162,500 pounds (73,709 kilograms). It required a ground run of 11,900 feet (3,627 meters), or 4,800 feet (1,463 meters) with JATO assist. The bomber could climb at a rate of 3,650 feet per minute (18.5 meters per second) at Sea Level, at combat weight and maximum power. The service ceiling was 37,500 feet (11,430 meters). The XB-47 carried 9,957 gallons (37,691 liters) of fuel. The combat radius was 1,175 nautical miles (1,352 statute miles/2,176 kilometers) with a 10,000 pound (4,536 kilogram) bomb load.

Planned armament (though the XB-47s were delivered without it) consisted of two .50-caliber machine guns in a tail turret, with 1,200 rounds of ammunition, and 10,000 pounds (4,536 kilograms) of bombs.

Boeing XB-47 Stratojet 46-065, the first of two prototypes, on the ramp at Boeing Field, Seattle, 1 December 1947. (U.S. Air Force)

The Stratojet was one of the most influential aircraft designs of all time and its legacy can be seen in almost every jet airliner built since the 1950s: the swept wing with engines suspended on pylons, mounted forward of the leading edge.

2,032 B-47s were built by Boeing Wichita, Douglas Tulsa and Lockheed Marietta. They served the United States Air Force from 1951 to 1977.

The very last B-47 flight took place 18 June 1986 when B-47E-25-DT, serial number 52-166, was flown from the Naval Air Weapons Center China Lake to Castle Air Force Base to be placed on static display.

XB-47 45-065 stalled while landing at Larson Air Force Base, near Moses Lake, Washington, 18 August 1951. The crew of three escaped uninjured. The airplane was damaged beyond repair. The second prototype, XB-47 46-066, is in the collection of the Air Force Flight Test Museum, Edwards Air Force Base, California.

Boeing XB-47 Stratojet 46-065. (U.S. Air Force)

© 2023, Bryan R. Swopes

11 December 1972 19:54:58 UTC, T plus 110:21:58

Astronaut Harrison H. Schmitt stands in front of the lunar lander Challenger (LM-12) and the lunar rover, 01:13:58 UTC, 12 December 1972. (Eugene A. Cernan/NASA)
Astronaut Harrison H. Schmitt stands in front of the lunar lander Challenger (LM-12) and the lunar rover, 01:13:58 UTC, 12 December 1972. (Eugene A. Cernan/NASA)

11 December 1972, 19:54:58 UTC: Apollo 17 lunar module Challenger with astronauts Eugene A. Cernan and Harrison H. Schmitt landed at the Taurus-Littrow Valley, The Moon.

Apollo 17 was the last manned moon mission.

Gene Cernan was the last human to stand on the lunar surface.

Astronaut Harrison H. Schmitt and the lunar rover at the edge of Shorty Crater in the Taurus-Littrow Valley, The Moon. (Eugene A. Cernan/NASA)
Astronaut Harrison H. Schmitt and the lunar rover at the edge of Shorty Crater in the Taurus-Littrow Valley, The Moon. (Eugene A. Cernan/NASA)

© 2015, Bryan R. Swopes

11 December 1959

Lieutenant General Joseph H. Moore (1914–2007)
Lieutenant General Joseph H. Moore, United States Air Force

11 December 1959: Brigadier General Joseph H. Moore, U.S. Air Force, Wing Commander, 4th Tactical Fighter Wing at Seymour Johnson Air Force Base, North Carolina, set a Fédération Aéronautique Internationale (FAI) World Speed Record when he flew a Republic F-105B-20-RE Thunderchief, serial number 57-5812, over a closed 100-kilometer (62.137 miles) closed course at Edwards Air Force Base, California. The Thunderchief averaged 1,878.67 kilometers per hour (1,167.35 miles per hour).¹ General Moore’s fighter bomber was a standard production aircraft and it was armed with a full load of ammunition for the M61 cannon.

FAI Record File Num #8873 [Direct Link]
Status: ratified – retired by changes of the sporting code
Region: World
Class: C (Powered Aeroplanes)
Sub-Class: C-1 (Landplanes)
Category: Not applicable
Group: 3 : turbo-jet
Type of record: Speed over a closed circuit of 100 km without payload
Performance: 1 878.67 km/h
Date: 1959-12-11
Course/Location: Edwards AFB, CA (USA)
Claimant Joseph H. Moore (USA)
Aeroplane: Republic F-105B
Engine: 1 Pratt & Whitney J-75

U.S. Air Force General Claims Air Speed Record Of 1,216 MPH

     LOS ANGELES (UPI)—Brig. Gen. Joseph H. Moore, a grandfather twice over, yesterday claimed a new world air speed record of 1,216 mph for the U.S. Air Force.

     Piloting a Republic F-105 Thunderchief jet, combat equipped, Moore broke the French record of 1,100.426 mph ² over a 100-kilometer closed course at Edwards Air force Base Friday.

     Moore emphasized at a press conference yesterday morning at International Airport here that the new mark has not yet been officially verified by the National Aeronautic Association.

      HE SAID he would attempt the flight again if the NAA does not recognize the new mark.

The general, a combat pilot with 100 missions during World War II who holds many decorations, said he broke the record twice Friday. His “slowest” speed was 1,170 miles an hour, some 70 miles an hour over the French record.

The record was run over the closed course which measured 100 kilometers, or 62.14 miles. He made most of the run at an altitude of 38,000 feet. The French run was made at about 2,500 feet,

     MOORE, 40, soft spoken with a faint Southern drawl, was met at the airport yesterday by his son, 1st Lt. Joseph Moore, a gunnery instructor with the Air Force at Williams Air Force Base, Ariz.

     The general stressed that his plane was a production model, equipped with ammunition and cannon just as it would be in combat. He said that some of the plane’s instruments had been removed to make room for scientific equipment.

     According to Moore, he actually hit a top speed of 1,400 miles an hour in “coming through the gate” at the end of his run around the circular course, about which he was guided by radio and scientific instruments.

The Arizona Republic, Sunday, December 13, 1959, Page 16, Columns 1-3

Republic F-105B-1-RE Thunderchief 54-102. (U.S. Air Force)
Republic F-105B-1-RE Thunderchief 54-102. (U.S. Air Force)

The F-105 was the largest single-seat, single-engine combat aircraft in history. It was designed as a tactical nuclear strike aircraft and fighter-bomber. The fuselage of the F-105B incorporated the “area rule” which gave the Thunderchief its characteristic “wasp waist” shape. The Thunderchief was 63 feet, 1 inch (19.228 meters) long with a wingspan of 34 feet, 11 inches (10.643 meters). It was 19 feet, 8 inches high (5.994 meters). wings were swept 45° at 25% chord. The angle of incidence was 0° and there was no twist. The wings had 3° 30′ anhedral. The total wing area was 385 square feet (35.8 square meters). The F-105 had an empty weight of 25,855 pounds (11,728 kilograms) and a maximum takeoff weight of 50,000 pounds (22,680 kilograms).

Brigadier General Joseph H. Moore with a Republic F-105 Thunderchief.
Brigadier General Joseph H. Moore with a Republic F-105 Thunderchief.

Early production F-105Bs had the Pratt & Whitney J75-P-5 axial-flow turbojet engine. Beginning with the Block 20 aircraft, the more powerful J75-P-19 was installed. The -19 engine was retrofitted to the earlier aircraft. The Thunderchief was powered by one Pratt & Whitney J75-P-19W engine. The J75 is a two-spool axial-flow afterburning turbojet with water injection. It has a 15-stage compressor section (8 low- and and 7 high-pressure stages) and 3-stage turbine section (1 high- and 2 low-pressure stages.) The J75-P-19W is rated at 14,300 pounds of thrust (63.61 kilonewtons), continuous power; 16,100 pounds (71.62 kilonewtons), Military Power (30-minute limit); and Maximum Power rating of 24,500 pounds (108.98 kilonewtons) with afterburner (15-minute limit). The engine could produce 26,500 pounds of thrust (117.88 kilonewtons) with water injection, for takeoff. The J75-P-19W is 21 feet, 7.3 inches (6.586 meters) long, 3 feet, 7.0 inches (1.092 meters) in diameter, and weighs 5,960 pounds (2,703 kilograms).

Armament consisted of one 20 mm General Electric M61 Vulcan six-barreled Gatling gun with 1,080 rounds of ammunition. It had an internal bomb bay and could carry bombs, missiles or fuel tanks on under wing and centerline hardpoints. The maximum bomb load consisted of fourteen 750-pound (340 kilogram) bombs. For tactical nuclear strike missions, the F-105B could carry one Mk 28 “special store” in the internal bomb bay.

The F-105B had a maximum speed of 737 knots (848 miles/1,364 kilometers per hour) at Sea Level, and 1,204 knots (1,386 miles per hour/2,230 kilometers per hour) at 35,000 feet (10,668 meters). The service ceiling was 45,700 feet (13,929 meters). Maximum range was 2,006 nautical miles (2,308 statute miles/3,715 kilometers).

Republic Aircraft Corporation built 833 Thunderchiefs for the U.S. Air Force. 75 of those were F-105Bs. 372 F-105s were lost to enemy action in South East Asia.

Republic F-105B-20-RE Thunderchief 57-5812 served with the 119th Tactical Fighter Squadron, New Jersey Air National Guard, and was later assigned to the 466th Tactical Fighter Squadron, 508th Tactical Fighter Wing at Hill Air Force Base, Utah. One source indicates that the the record-setting F-105B was used as a battle damage repair trainer at McClellan Air Force Base, Sacramento, California, from October 1980.

Six F-105B-10-REs (6 of 9 block 10 aircraft built) of General Moore's 4th Tactical Fighter Wing parked on the ramp. The stripes on the nose and vertical fin are green. Aircraft are (nearest to farthest) S/N 57-5779, -5780, -5782, -5784, -5781, -5778. (U.S. Air Force photo)
Six F-105B-10-REs (6 of 9 block 10 aircraft built) of General Moore’s 4th Tactical Fighter Wing parked on the ramp. The stripes on the nose and vertical fin are green. Aircraft are (nearest to farthest) 57-5779, -5780, -5782, -5784, -5781, -5778. (U.S. Air Force)
Three Republic F-105B-20-RE Thunderchiefs, serial numbers 57-5815, 57-5807 and 57-5822, begin their takeoff roll. This is the same block number as the F-105B flown by General Moore for the FAI World Speed Record. (U.S. Air Force)
Three Republic F-105B-20-RE Thunderchiefs, serial numbers 57-5815, 57-5807 and 57-5822, begin their takeoff roll. These are from the same production block as the F-105B flown by General Moore for the FAI World Speed Record. (U.S. Air Force)
Republic F-105B-20-RE Thunderchief 57-5812, assigned to the 466th Tactical Fighter Squadron. (Million Monkey Theater)
The World Speed Record holder, Republic F-105B-20-RE Thunderchief 57-5812, assigned to the 466th Tactical Fighter Squadron, 508th Tactical Fighter Wing, Hill Air Force Base, Utah. (Million Monkey Theater)

¹ Many sources, including the newspaper article quoted above, cite General Moore’s World Record Speed for the 100-kilometer closed course at 1,216.48 miles per hour (1,957.745 kilometers per hour). The FAI’s official web site gives General Moore’s speed as 1,878.67 kilometers per hour (1,167.35 miles per hour). (See above.) Also, many sources (including General Moore’s official Air Force biography) state that General Moore won the Bendix Trophy for this flight. The Bendix Trophy was awarded to the winner of an annual West-to-East transcontinental air race. The Smithsonian Institution indicates that the Bendix Trophy was not awarded for the years 1958, 1959 or 1960.

² FAI Record File Number 8874, 1 771 km/h, set 18 June 1959 by Gérard Muselli, flying a Dassault Mirage III A over Brétigny-sur Orge, France.

© 2018, Bryan R. Swopes

11 December 1951

Test pilot William R. Murray at the control of Kaman K-225, Bu. No. 125477, with a Boeing 502-2 gas turbine engine installed. (U.S. Navy)

11 December 1951: The first helicopter powered by a gas turbine engine made its first flight at the Kaman Aircraft Company plant at Bloomfield, Connecticut. Using a K-225 tandem rotor helicopter delivered to the U.S. Navy in 1949, Bureau of Aeronautics serial number (“Bu. No.”) 125477, Kaman replaced the 220 horsepower Lycoming O-435-A2 reciprocating engine with a Boeing 502-2E turboshaft engine. This engine could produce 175 continuous horsepower at 2,900 r.p.m. at Sea Level, less than the piston engine it replaced, but it also weighed considerably less.

K-225 Bu. No. 125477 was the first helicopter to perform an intentional loop, when it was delivered to the Navy at NATC Patuxent River by factory test pilot William R. Murray. It was placed in storage at Bradley Field, Windsor Locks, Connecticut until 1957. The gas turbine had been removed. When the helicopter was transferred to the Smithsonian Institution in 1957, a similar-appearing Boeing YT-50-BO-2 gas turbine engine was installed.

The K-225 was a two-place, single-engine helicopter using Kaman’s unique system of counter-rotating, intermeshing rotors (“synchropter”). Each rotor cancelled the torque reaction of the other, eliminating the need for a tail rotor. In a conventional single-rotor helicopter, up to 30% of the engine power is required to drive the tail rotor. With the counter-rotating design, the total engine power is available for lift and thrust.

K-225 Bu. No. 125477 is 22 feet, 5 inches (6.83 meters) long. Each rotor has a diameter of 38 feet (11.58 meters). It stands 11 feet, 6 inches (3.51 meters) high. The helicopter has an empty weight of 1,800 pounds (816 kilograms) and a maximum gross weight of 2,700 pounds (1,225 kilograms). It is a slow helicopter, with a never-exceed (VNE) limit of 70 miles per hour (112.7 kilometers per hour). This historic helicopter is on display at the Smithsonian Institution National Air and Space Museum, Steven F. Udvar-Hazy Center in Chantilly, Virginia.

Kaman K-225, Bu. No. 125477, the first gas turbine-powered helicopter, at the Vertical Flight Gallery, Steven F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum, Chantilly, Virginia. (NASM)
Kaman K-225, Bu. No. 125477, the first gas turbine-powered helicopter, at the Vertical Flight Gallery, Steven F. Udvar-Hazy Center, Smithsonian Institution National Air and Space Museum, Chantilly, Virginia. (NASM)

© 2016, Bryan R. Swopes

11 December 1945

Bell-Atlanta B-29B-60-BA Superfortress 44-84061, the Pacusan Dreamboat. (U.S. Air Force)
Bell-Atlanta B-29B-60-BA Superfortress 44-84061, the Pacusan Dreamboat. (U.S. Air Force)

11 December 1945: Three days after Lieutenant Colonel Henry E. Warden and Captain Glen W. Edwards set a transcontinental speed record flying a prototype Douglas XB-42 from Long Beach, California, to Washington, D.C., in 5 hours, 17 minutes, Colonel Clarence S. Irvine and the crew of the B-29 Pacusan Dreamboat also set a record, flying from Burbank, California to overhead Floyd Bennett Field, New York, in 5 hours, 27 minutes, 8 seconds. The average speed for the 2,464-mile flight was 450.38 miles per hour (724.82 kilometers per hour).

Lieutenant General Clarence S. Irvine, U.S. Air Force

Irvine was Deputy Chief of Staff, Pacific Air Command, 1944–1947. He flew the Pacusan Dreamboat on several record-setting flights, including Guam to Washington, D.C., and Honolulu, Hawaii to Cairo, Egypt. He rose to the rank of lieutenant general in the United States Air Force, and served as Deputy Chief of Staff for Materiel.

Pacusan Dreamboat was a Bell Aircraft Corporation B-29B-60-BA Superfortress, built at Marietta, Georgia. The B-29B was a lightweight variant of the B-29, intended for operation at lower altitudes. It did not have the four power gun turrets and their .50-caliber machine guns. A radar-directed 20 mm cannon and two .50-caliber machine guns in the tail were the only defensive weapons. Much of the standard armor plate was also deleted. Pacusan Dreamboat was further lightened. The tail guns were removed and the tail reshaped.

The B-29B was equipped with four air-cooled, fuel-injected Wright R-3350-CA-2 Duplex Cyclone two-row 18 cylinder radial engines and specially-designed propellers. The engine nacelles were modified for improved cooling.

The Superfortress had been lightened to an empty weight of 66,000 pounds (29,937 kilograms). A standard B-29B weighed 69,000 pounds (31,298 kilograms) empty and 137,000 pounds (62,142 kilograms) fully loaded. Additional fuel tanks installed on the Dreamboat were able to carry 10,000 gallons (37,854 liters) of gasoline.

Colonel Clarence S. Irvine (standing, left) with the crew of Pacusan Dreamboat: W.J.Benett, G.F.Broughton, Dock West, W.S. O’Hara, F.S. O’Leary, K.L. Royer, F.J.Shannon, J.A. Shinnault, G.R. Stanley. (FAI)
Colonel Clarence S. Irvine (standing, left) with the crew of Pacusan Dreamboat: W.J. Benett, G.F. Broughton, Dock West, W.S. O’Hara, F.S. O’Leary, K.L. Royer, F.J. Shannon, J.A. Shinnault, G.R. Stanley. (FAI)

© 2015, Bryan R. Swopes