Tag Archives: Rocket

8 September 1944

V-2 crater at Staveley Road, 8 September 1944. (Daily Mail)
V-2 crater at Staveley Road, 8 September 1944. (Daily Mail)
The first V-2 rocket to hit London impacted in Staveley Road at 18:40:52, 8 September 1944, killing 3 persons and injuring 17 others.
The first V-2 rocket to hit London impacted in Staveley Road at 18:40:52, 8 September 1944, killing 3 persons and injuring 17 others.

8 September 1944: At 18:40:52 hours, the first of 1,358 V-2 rockets hit London, impacting in Staveley Road, Chiswick, “opposite No. 5.”

The warhead detonated and caused extensive damage to the residential area. A crater 20 feet (6.1 meters) deep was in the center of the road and the gas and water mains were  destroyed.

This V-2 rocket was fired by Gruppe Nord, Battery 2./485, located at the crossroads of Lijsterlaan and Schouwweg, in the suburb of Wassenar, The Hague, Netherlands.

Three people were killed: a 67-year-old woman, a 3-year-old child and a soldier home on leave. 17 others were injured.

11 homes were demolished, 12 seriously damaged and unusable, and 556 suffered slight or minor damage. 14 families had to be relocated.

A V-2 rocket is being raised to a vertical position for firing.
A V-2 rocket is being raised to a vertical position for firing.

The V2, or Vergeltungswaffen 2 (also known as the A4, or Aggregat 4) was a ballistic missile with an empty weight of approximately 10,000 pounds (4,536 kilograms) and weighing 28,000 pounds (12,700 kilograms), fully loaded. It carried a 738 kilogram (1,627 pound) (sources vary) explosive warhead of amatol, a mixture of ammonium nitrate and TNT. The propellant was a 75/25 mixture of ethanol and water with liquid oxygen as an oxidizer.

1280px-esquema_de_la_v-2The complete rocket was 14.036 meters (46.050 feet) long, and had a maximum diameter of 1.651 meters (5.417 feet). The rocket was stabilized by four large fins, 3.945 meters (12.943 feet) long, with a maximum span of  3.564 meters (11.693 feet). The leading edge of these fins was swept aft 60° to the “shoulder,” and then to 87° (30° and 3°, relative to the rocket’s centerline). A small guide vane was at the outer tip of each fin, and other vanes were placed in the engine’s exhaust plume.

V-2 launch site.
V-2 launch site.

When launched, the rocket engine burned for 65 seconds, accelerating the rocket to 3,580 miles per hour (5,760 kilometers per hour) on a ballistic trajectory. The maximum range of the rocket was 200 miles (320 kilometers) with a peak altitude between 88 and 128 miles, depending on the desired range. On impact, the rocket was falling at 1,790 miles per hour (2,880 kilometers per hour), about Mach 2.35, so its approach would have been completely silent in the target area.

The V-2 could only hit a general area and was not militarily effective. Germany used it against England, France, The Netherlands and Belgium as a terror weapon. More than 3,200 V-2 rockets were launched against these countries.

V-2 rockets on mobile launchers being prepared for firing. (Bildarchiv Preussischer Kulturbesitz)

© 2016, Bryan R. Swopes

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20 August 1977

Voyager 2/Titan IIIE-Centaur launch, LC-41, Kennedy Space Center, Florida, 20 August 1977. (NASA)

20 August 1977: Voyager 2 was launched from Launch Complex 41 at the Kennedy Space Center, Cape Canaveral, Florida, aboard a Titan IIIE-Centaur launch vehicle. It was placed on an orbital trajectory that would take it on a journey throughout the Solar System and beyond.

Nearly two years later, 9 July 1979, Voyager 2 made its closest approach to Jupiter, passing within 350,000 miles (570,000 kilometers) of the planet. Many dramatic images as well as scientific data were transmitted back to Earth.

Artist’s concept of Voyager. (NASA/JPL)

The probe continued outward to Saturn, Neptune and Uranus, continuously transmitting images and data. In 1990, the space probe passed beyond the limits of the Solar System.

Voyager 2 is now approaching interstellar space. It is still transiting the heliosheath, where “solar wind” is slowed by the pressure of interstellar gas. (10,706,654,718 miles, or 17,230,690,530 kilometers, from the Sun, as of 17:22:00 hours, PDT, 19 August 2017) and is still operating, 40 years after it was launched.

Voyager 2 captured this image of the moon Io transiting Jupiter, 9 July 1979. (NASA)
Uranus, imaged by Voyager 2, 24 January 1986. (NASA/JPL–Caltech)
This image of Neptune was captured by Voyager 2 on 20 August 1989, 28 years ago. (NASA)

© 2017, Bryan R. Swopes

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20 August 1975

Viking 1/Titan IIIE-Centaur launches from Kennedy Space Centaur, enroute to Mars, 20 August 1975. (NASA)

20 August 1975: The Viking 1 space probe was launched from Kennedy Space Center, Cape Canaveral, Florida, aboard a Titan IIIE/Centaur rocket. For the next ten months it traveled to Mars, the fourth planet of the Solar System. Once there, it was placed in orbit and began sending telemetry data back to Earth. A Viking Lander descended to the planet’s surface, landing at Chryse Planitia.

This was the first time that a spacecraft had landed on another planet. The orbiter continued to operate over the course of 1,485 orbits. As it ran low on fuel, mission controllers boosted it into a higher orbit to prevent it falling to the planet. Orbiter operations were terminated 17 August 1980. The lander operated for 6 years, 116 days, before the mission was terminated by a faulty transmission which resulted in a loss of contact, 11 November 1982.

The surface of Chryse Planitia, Mars, photographed by the Viking 1 Lander. (NASA)

© 2015, Bryan R. Swopes

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28 March 1935

Dr. Robert H. Goddard with one of his liquid-fueled A-series rockets at Roswell, New Mexico, circa 1935. (National Air and Space Museum Archives, Smithsonian Institution, Image Number 84-8949)
Dr. Robert H. Goddard with one of his liquid-fueled A-series rockets at Roswell, New Mexico, circa 1935. (National Air and Space Museum Archives, Smithsonian Institution)

28 March 1935: Near Roswell, New Mexico, Robert H. Goddard successfully launched the first gyroscopically-stabilized liquid-fueled rocket. In a 20-second flight, the A Series rocket, number A-5, reached an altitude of 4,800 feet (1,463 meters) and traveled 13,000 feet (3,962 meters) down range. Its speed was 550 miles per hour (885 kilometers per hour). During the flight, the rocket corrected its flight path several times.

"Dr. Robert H. Goddard observes the launch site from his launch control shack while standing by the firing control panel. From here he can fire, release, or stop testing if firing was unsatisfactory. Firing, releasing, and stop keys are shown on panel. The rocket is situated in the launch tower." (NASA)
“Dr. Robert H. Goddard observes the launch site from his launch control shack while standing by the firing control panel. From here he can fire, release, or stop testing if firing was unsatisfactory. Firing, releasing, and stop keys are shown on panel. The rocket is situated in the launch tower.” (U.S. Air Force)
Goddard A-series rocket. (Clark University)

The A Series rockets were of varying lengths and mass. The representative A-series rocket displayed at the National Air and Space Museum is 15 feet, 4½ inches (468.63 centimeters) long with a diameter of 9 inches (22.86 centimeters). The span across the fins is 1 foot, 9½ inches (54.61 centimeters). It weighs 78.5 pounds (35.6 kilograms). The rocket was fueled with gasoline and liquid oxygen, pressurized with nitrogen.

A gyroscope controlled vanes placed in the engine’s exhaust, providing stabilization during powered flight.

Goddard flew the A-sereies 14 times between 15 January and 29 October 1935.

The National Air and Space Museum describes the rocket’s construction:

“Aluminum skin, thin gauge, a long tail section from bottom of fins to bottom of mid-section. Aluminum skin also on parachute section and nosecone wholly of spun aluminum except for steel attachment screw. Steel skin (for greater strength and insulation) below nosecone, over mid-section (over propellant tanks), and around small section above fins. One steel tube or pipe on each side of rocket, along propellant section; one smaller diameter copper tube on one side. Steel nozzle and other interior components. Fabric parachute.”

Goddard is the “Father of Modern Rocketry.” Many of his developments were copied by German engineers as they developed the V2 rocket of World War II. And this led to America’s own post-War rocket developments, including the mighty Saturn V moon rocket.

This photograph, taken at the launch site, shows Dr. Goddard with his supporters and his assistants. Left to Right: Albert Kisk, Harry F. Guggenheim, Dr. Goddard, Charles A. Lindbergh, Nils T. Ljungquist and Charles Mansur. (U.S. Air Force)
This photograph, taken at the launch site in New Mexico, shows Dr. Goddard with his supporters and his assistants. Left to Right: Albert Kisk, machinist; Harry F. Guggenheim, philanthropist; Dr.Robert H. Goddard; Charles A. Lindbergh, aviator; Nils T. Ljungquist, machinist; and Charles Mansur, a welder. (U.S. Air Force)
A 1935 A-Series rocket at the National Air and Space Museum, donated by Dr. Robert H. Goddard. (NASM)
A 1935 A-Series rocket at the National Air and Space Museum, donated by Dr. Robert H. Goddard. It is constructed from parts of several A-series rockets which had been test flown. (NASM)

© 2019, Bryan R. Swopes

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