Tag Archives: Douglas Aircraft Company

10 July 1962

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Telstar 1 launches aboard a Thor Delta rocket at Launch Complex 17B, 0835 GMT, 10 July 1962. (NASA)
Telstar 1 launches aboard a Delta rocket at Launch Complex 17B, 0835 GMT, 10 July 1962. (NASA)

10 July 1962: At 0835 GMT (4:35 a.m., EDT) the first communications relay satellite, Telstar 1, was launched into Earth orbit from Launch Complex 17B, Cape Canaveral Air Force Station, Florida. The launch vehicle was a three-stage liquid-fueled Delta rocket.

This was the first commercial space flight, sponsored by a consortium of communications companies and government organizations, including AT&T, Bell Labs, the BBC, NASA, and British and French postal services. The satellite was used to relay live television broadcasts across the Atlantic Ocean. This had never previously been possible.

Telstar weighed 171 pounds (77.5 kilograms). Its weight and size were restricted by the availability of launch vehicles. The satellite was placed in an elliptical orbit, varying from 591 miles (952 kilometers) to 3,686 miles (5,933 kilometers), and inclined at about a 45° angle to Earth’s Equator. The orbital period was 2 hours, 37 minutes. The properties of Telstar’s orbit restricted its use to about 20 minutes during each pass.

In addition to its primary role as a communications relay satellite, Telstar also performed scientific experiments to study the Van Allen Belt.

The Delta was a three-stage expendable launch vehicle which was developed from the Douglas Aircraft Company’s SM-75 Thor intermediate-range ballistic missile.

Designated Thor DM-19, the first stage was 60.43 feet (18.42 meters) long and 8 feet (2.44 meters) in diameter. Fully fueled, the first stage had a gross weight of 108,770 pounds (49,337 kilograms). It was powered by a Rocketdyne LR-79-7 engine which burned liquid oxygen and RP-1 (a highly-refined kerosene rocket fuel) and produced 170,565 pounds of thrust (758.711 kilonewtons). This stage had a burn time of 2 minutes, 45 seconds.

The second stage was an Aerojet General Corporation-built Delta 104. It was 19 feet, 3 inches (5.88 meters) long with a maximum diameter of 4 feet, 6 inches (1.40 meters). The second stage had a gross weight of 9,859 pounds (4,472 kilograms). It used an Aerojet AJ10-104 rocket engine which burned a hypergolic  mixture of nitric acid and UDMH. The second stage produced 7,890 pounds of thrust (35.096 kilonewtons) and burned for 4 minutes, 38 seconds.

The third stage was an Allegany Ballistics Laboratory Altair 1. It was 6 feet long, 1 foot, 6 inches in diameter and had a gross weight of 524 pounds (238 kilograms). This stage used a solid-fuel Thiokol X-248 rocket engine, producing 2,799 pounds of thrust (12.451 kilonewtons). Its burn time was 4 minutes, 16 seconds.

The three stages of the Delta rocket accelerated the Telstar satellite to 14,688 miles per hour for orbital insertion.

The day prior to launch, the United States detonated a 1.45 megaton thermonuclear warhead at an altitude of 248 miles (400 kilometers), near Johnston Island in the Pacific Ocean. (Operation Dominic-Fishbowl Starfish Prime). Between 21 October 1961 and 1 November 1962, the Soviet Union detonated five nuclear warheads in space (Project K), at altitudes ranging from 59 to 300 kilometers (37–186 miles) over a test range in Khazakhstan. High energy electrons from these tests were trapped in the Earth’s radiation belts. This damaged the satellite’s circuitry and it went out of service in December 1962. ¹

Engineers were able to work around the damage and restore service by January 1963, but Telstar 1 failed permanently 21 February 1963.

Telstar is still in Earth orbit.

Telstar 1 communications relay satellite. (Bell Laboratories)

¹ Thanks to regular TDiA reader Steve Johnson for this information.

© 2019, Bryan R. Swopes

10 July 1942

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Douglas XA-26 first flight, 10 July 1942. (Boeing Historical Archives/Wikipedia)

10 July 1942: At the Douglas Aircraft Company El Segundo Division, located at the southeast section of Los Angeles Municipal Airport (now, LAX), company engineering test pilot Benjamin Odell Howard took the prototype Douglas XA-26-DE light bomber, serial number 41-19504,¹ for its first flight.

Douglas XA-26 prototype in flight. (Douglas Aircraft Company/SDASM)

The XA-26 was twin-engine mid-wing monoplane with retractable tricycle landing gear. Douglas had proposed the design to the U.S. Army Air Corps as a replacement for three different airplanes: The Douglas A-20, the North American Aviation B-25 Mitchell, and the Martin B-26 Marauder. It was to be operated by a pilot, navigator/bombardier and a gunner.

Douglas XA-26.

The prototype was 51 feet, 2 inches (15.596 meters) long, with a wingspan of 70 feet, 0 inches (21.336 meters) and overall height of 18 feet, 6 inches (5.639 meters). Its empty weight was 21,150 pounds. It was powered by two air-cooled, supercharged, Pratt & Whitney R-2800–27 (Double Wasp 2SB-G), with a normal power rating of 1,600 horsepower at 2,400 r.p.m. to 5,700 feet (1,737 meters) and 1,450 horsepower to 13,000 feet (3,962 meters); and 2,000 horsepower at 2,700 r.p.m., for military and takeoff power. The engines drove three-bladed propellers through a 2:1 gear reduction. The R-2800-27 was 6 feet, 3.72 inches (1.923 meters) long, 4 feet, 4.50 inches (1.334 meters) in diameter and weighed 2,300 pounds (1,043 kilograms).

Douglas XA-26 (Douglas Aircraft Company/SDASM)

The XA-26’s maximum speed was 322 knots (370 miles per hour/595 kilometers per hour) at 17,000 feet (5,182meters) and it had a service ceiling of 31,300 feet (9,540 meters).

Douglas XA-26 light bomber prototype, 42-19504. (Douglas Aircraft Company)

A second prototype, designated XA-26A was developed as an night fighter. It carried air-intercept radar in the nose and armament in a pod under the fuselage. The third prototype, the XA-26B, was a ground attack aircraft. Like the XA-26A, it had a solid nose, but was armed with a fixed 75-millimeter cannon in the nose, and forward-firing Browning .50-caliber machine guns. When ordered into production, the XA-26 became the A-26C Invader, while the ground attack design was assigned A-26B.

Douglas XA-26A night fighter prototype, 42-19505, photographed 6 July 1943. Note the weapons pod beneath the fuselage. (Douglas Aircraft Company/SDASM)
Douglas XA-26B ground attack prototype, 42-19588, photographed 14 May 1943. (Douglas Aircraft Company E.S. 31578/Boeing Historical Archives)
Douglas XA-26 42-19504, photographed 29 April 1943. (Douglas Aircraft Company/SDASM)

Benjamin Odell Howard was born 4 February 1904 at Palestine, Texas. He was the third of four children of Sam T. Howard, a real estate agent, and Fanie Howard.

Ben O. Howard, 1924 (The Savitar)

Ben Howard graduated from the University of Missouri at Columbia in 1924 with a degree in engineering. While there he was a member of the Kappa Sigma (ΚΣ) fraternity and the Reserve Officers Club.

On 10 Dec 1932, Howard married Miss Olive Maxine Schoen at Independence, Missouri.

In 1933, they lived in Kansas City, Missouri. He was employed as a pilot for United Air Lines Inc.

In 1935, Ben Howard won the Bendix Trophy Race flying Mister Mulligan, a Howard DGA-6. His time was 8 hours, 33 minutes, 16.3 seconds, for an average speed of 238.70 miles per hour.

Mister Mulligan, the Howard DGC-6, NR273Y. (SDASM)

On his 1940 Selective Service (conscription, or draft) card, Howard was described as having a dark complexion, black hair and brown eyes. He was 5 feet, 11 inches (180 centimeters) tall, and weighed 165 pounds (75 kilograms).

After a lengthy illness, Benjamin Odell Howard died at his home in Brentwood, California, 4 December 1970.

¹ Every source checked by TDiA identifies the prototype XA-26 as “41-19504.” Photographs of the XA-26, XA-26A and XA-26B clearly show the 1942 serial numbers 219504, 219505 and 219588 (42-19504, 42-19505 and 42-19588).

© 2019, Bryan R. Swopes

9 July 1962, 09:00:09 UTC, T + 13:41

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Fireball of Operation Dominic-Fishbowl Starfish Prime, 248 miles (399.1 kilometers) above the Pacific Ocean, 9 July 1962. (U.S. Department of Defense)

9 July 1962: At 09:00:09 UTC, the United States detonated a thermonuclear warhead over the Pacific Ocean. This was part of the Operation Dominic-Fishbowl test series at Johnston Island, and was designated Starfish Prime.

A Thor missile is launched from Johnston Island. Note the instrumentation pods at the base of the rocket. (Johnston Memories)

At 08:46:28 UTC, a Douglas Thor DSV2E orbital launch vehicle, serial number 195,  was launched from missile complex LE-1 on Johnston Island, carrying a W-49 warhead in an AVCO Corporation Mk-2 reentry vehicle. The rocket also carried three instrumentation pods which were jettisoned at pre-selected altitudes. The W-49 reached a peak altitude of 600 miles (965 kilometers) along a ballistic trajectory, and then began to descend.

Starfish Prime fireball was visible from Honolulu, Oahu, Hawaii, 898 miles (1,445.2 kilometers) from Ground Zero. “Widespread red air glow (6300 å) amid dark clouds, caused mostly by x-ray-excited atomic oxygen (i.e., oxygen by photoelectrons liberated by Starfish X-rays)” (Commission to Assess Threat to the United States from Electromagnetic Pulse (EMP) Attack, 2004, at Page 5)
Starfish Prime (atomicarchive.com)

The W-49 detonated 36 kilometers (22 miles) southwest of Johnston Island at an altitude of 400 kilometers (246 miles) with an explosive yield of 1.45 megatons. The point of detonation deviated from the planned Air Zero by 1,890 feet (576 meters) to the north, 2,190 feet (668 meters) east, and +617 feet (188 meters) in altitude. The fireball was clearly visible in the Hawaiian Islands, more than 800 miles (1,288 kilometers) away.

The electromagnetic pulse (EMP) damaged electrical systems in The Islands, cutting power, damaging equipment and interrupting telephone systems. Brilliant auroras were visible, lasting about 7 minutes.

Telstar, an American communications satellite that was placed in Earth orbit the following day, was also damaged by residual radiation from the detonation.

The Starfish Prime experiment was for the purpose of “Evaluation of missile kill mechanisms produced by a high altitude nuclear detonation.” The electromagnetic effects on communications were also studied.

A Douglas SM-75/PGM-17A Thor IRBM. (U.S. Air Force)
A Douglas SM-75 Thor IRBM (DM-18A) is launched at Launch Complex 17B, Cape Canaveral Air Force Station, Florida, 12 May 1959. (U.S. Air Force)

The Thor DSV2E was an orbital launch variant of the Douglas Aircraft Company SM-75 Thor IRBM. This was a single-stage nuclear-armed intermediate-range ballistic missile, 61 feet, 3.91 (19.692 meters) long and 8 feet, 0.00 inches (2.438 meters) in diameter. With the Mk-2 reentry vehicle, the overall length of the missile was 63 feet, 7.38 inches (19.390 meters). It weighed 109,800 pounds (49,805 kilograms) at liftoff and 6,889 pounds (3,124 kilograms) at burnout.

The SM-75 was powered by one Rocketdyne LR79-NA-9 rocket engine which produced 150,000 pounds of thrust (667.23 kilonewtons). Two Rocketdyne LR101-NA-9 vernier engines of 1,000 pounds thrust (4.45 kN), each, provided directional control and thrust adjustments. The Thor was fueled with kerosene and liquid oxygen sufficient for 156 seconds of main engine burn time.

The Thor could reach a maximum speed of 11,020 miles per hour (17,735 kilometers per hour) and had a maximum range of 1,500 miles (2,414 kilometers).

The W-49 thermonuclear warhead was designed by the Los Alamos Scientific Laboratory (LASL) and is believed to be a development of the earlier B-28 two-stage radiation-implosion bomb. It incorporated a 10-kiloton W-34 warhead as a gas-boosted fission primary, and had a one-point-safe safety system. The warhead had a diameter of 1 foot, 8 inches (0.508 meters) and length of  4 feet, 6.3 inches (1.379 meters). It weighed 1,665 pounds (755 kilograms).

The flash from the Starfish-Prime detonation, photographed from Maui in the Hawaiian Islands 15 seconds after detonation. (Los Alamos National Laboratory)
The flash from the Starfish-Prime detonation, photographed from Maui in the Hawaiian Islands, 15 seconds after detonation. (Los Alamos National Laboratory)

© 2020, Bryan R. Swopes