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Archive for 2019

August 27, 2019

Delta IV GPS III SV-2 Launch

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Wikipedia dicit:

Delta IV is a group of five expendable launch systems in the Delta rocket family introduced in the early 2000s. Originally designed by Boeing’s Defense, Space & Security division for the Evolved Expendable Launch Vehicle (EELV) program, the Delta IV became a United Launch Alliance (ULA) product in 2006. The Delta IV was and is primarily a launch vehicle for United States Air Force military payloads, but has also been used to launch a number of U.S. government non-military payloads and a single commercial satellite.

The Delta IV originally had two main versions which allowed the family to cover a range of payload sizes and masses: the retired Medium (which had four configurations) and Heavy. As of 2019, only the Heavy remains active, with payloads that would previously fly on Medium moving to either the existing Atlas V or the forthcoming Vulcan. Retirement of the Delta IV is anticipated in 2024.

Delta IV vehicles are built in the ULA facility in Decatur, Alabama. Final assembly is completed at the launch site by ULA: at the Horizontal Integration Facility for launches from SLC-37B at Cape Canaveral and in a similar facility for launches from SLC-6 at Vandenberg Air Force Base.

Video Credit: ULA

 

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August 26, 2019

Soyuz MS-14 Rollout and Launch

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Wikipedia dicit:

The Soyuz launcher was introduced in 1966, deriving from the Vostok launcher, which in turn was based on the 8K74 or R-7a intercontinental ballistic missile. It was initially a three-stage rocket with a Block I upper stage. Later a Molniya variant was produced by adding a fourth stage, allowing it to reach the highly elliptical molniya orbit. A later variant was the Soyuz-U. While the exact model and variant designations were kept secret from the west, the Soyuz launcher was referred to by either the United States Department of Defense designation of SL-4, or the Sheldon designation of A-2 (developed by Charles S. Sheldon, an analyst with the Library of Congress). Both systems for naming Soviet rockets stopped being used as more accurate information became available.

The production of Soyuz launchers reached a peak of 60 per year in the early 1980s. It has become the world’s most used space launcher, flying over 1700 times, far more than any other rocket. Despite its age and perhaps thanks to its simplicity, this rocket family has been notable for its low cost and high reliability.

Video Credit: Roscosmos

 

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August 22, 2019

Biomining

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NASA dicit:

As humans plan expeditions to places such as the Moon and Mars, biomining could offer a way to obtain needed materials on other planetary bodies rather than bringing them from Earth. However, microbes and rocks interact differently outside of Earth’s gravity, potentially affecting output from extraterrestrial biomining. A new investigation on the International Space Station is studying how microbes grow on and alter planetary rocks in microgravity and simulated Martian gravity.

Video Credit: NASA Johnson

 

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August 21, 2019

Spica RCS

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Copenhagen Suborbitals dicit:

Adrian guides you through his project of a Reaction Control System for our crewed Spica space capsule. This system will enable our spacecraft to orient and stabilize itself in the vacuum of space.

Copenhagen Suborbitals is the world’s only manned, amateur space program, 100% crowdfunded and nonprofit. In the future, one of us will fly to space on a home built rocket.

Video Credit: Copenhagen Suborbitals

 

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August 20, 2019

Soyuz MS-14 Assembly

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Wikipedia dicit:

A Soyuz spacecraft consists of three parts (from front to back): a spheroid orbital module, which provides accommodation for the crew during their mission; a small aerodynamic reentry module, which returns the crew to Earth; a cylindrical service module with solar panels attached, which contains the instruments and engines.

The orbital and service modules are single-use and are destroyed upon reentry in the atmosphere. Though this might seem wasteful, it reduces the amount of heat shielding required for reentry, saving mass compared to designs containing all of the living space and life support in a single capsule. This allows smaller rockets to launch the spacecraft or can be used to increase the habitable space available to the crew (6.2 m3 or 220 cu ft in Apollo CM vs 7.5 m3 or 260 cu ft in Soyuz) in the mass budget. The orbital and reentry portions are habitable living space, with the service module containing the fuel, main engines and instrumentation.

Soyuz can carry up to three crew members and provide life support for about 30 person days. The life support system provides a nitrogen/oxygen atmosphere at sea level partial pressures. The atmosphere is regenerated through potassium superoxide (KO2) cylinders, which absorb most of the carbon dioxide (CO2) and water produced by the crew and regenerates the oxygen, and lithium hydroxide (LiOH) cylinders which absorb leftover CO2.

The vehicle is protected during launch by a payload fairing, which is jettisoned along with the SAS at ​2 1â„2 minutes into launch. It has an automatic docking system. The ship can be operated automatically, or by a pilot independently of ground control.

Video Credit: Roscosmos

 

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August 15, 2019

Solar Wind Animation

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Wikipedia dicit:

The solar wind is a stream of charged particles released from the upper atmosphere of the Sun, called the corona. This plasma mostly consists of electrons, protons and alpha particles with kinetic energy between 0.5 and 10 keV. Embedded within the solar-wind plasma is the interplanetary magnetic field. The solar wind varies in density, temperature and speed over time and over solar latitude and longitude. Its particles can escape the Sun’s gravity because of their high energy resulting from the high temperature of the corona, which in turn is a result of the coronal magnetic field.

At a distance of more than a few solar radii from the Sun, the solar wind is supersonic and reaches speeds of 250 to 750 kilometers per second. The flow of the solar wind is no longer supersonic at the termination shock. The Voyager 2 spacecraft crossed the shock more than five times between 30 August and 10 December 2007. Voyager 2 crossed the shock about a billion kilometers closer to the Sun than the 13.5-billion-kilometer distance where Voyager 1 came upon the termination shock. The spacecraft moved outward through the termination shock into the heliosheath and onward toward the interstellar medium. Other related phenomena include the aurora (northern and southern lights), the plasma tails of comets that always point away from the Sun, and geomagnetic storms that can change the direction of magnetic field lines.

Video Credit: NASA’s Goddard Space Flight Center/Conceptual Image Lab/Krystofer Kim (USRA): Animator

 

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