#building

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

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  • Prompt: With lift-off mass of 210,000 kg (460,000 lb), Ariane 1 was able to put in geostationary transfer orbit one satellite or two smaller of a maximal weight of 1,850 kg (4,080 lb). The cost of program is estimated at 2 billion euros. The Ariane 1 was a four-stage vehicle (fourth stage put satellite from GTO to GEO is usually not counted as part of rocket, because it is included in 1,850 kg of payload). The first stage was equipped with 4 Viking engines developed by the Société Européenne de Propulsion. The second stage had a single Viking engine. The third stage had one LOX/LH2 bipropellant engine capable of a thrust of 7,000 kgf (69 kN; 15,000 lbf). This design was kept in the Ariane series until Ariane 4.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: A space station is a spacecraft capable of supporting a human crew in orbit for an extended period of time, and is therefore a type of space habitat. It lacks major propulsion or landing systems. An orbital station or an orbital space station is an artificial satellite (i.e. a type of orbital spaceflight). Stations must have docking ports to allow other spacecraft to dock to transfer crew and supplies. The purpose of maintaining an orbital outpost varies depending on the program. Space stations have most often been launched for scientific purposes, but military launches have also occurred.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The ziggurat was built by King Ur-Nammu, who dedicated it in honour of Nanna/Sîn in approximately the 21st century BC (short chronology) during the Third Dynasty of Ur. The massive step pyramid measured 64 m (210 ft) in length, 45 m (148 ft) in width and over 30 m (98 ft) in height. The height is speculative, as only the foundations of the Sumerian ziggurat have survived. The ziggurat was a piece in a temple complex that served as an administrative center for the city, and which was a shrine of the moon god Nanna, the patron deity of Ur. The construction of the ziggurat was finished in the 21st century BC by King Shulgi, who, in order to win the allegiance of cities, proclaimed himself a god. During his 48-year reign, the city of Ur grew to be the capital of a state controlling much of Mesopotamia. Many ziggurats were made by stacking mud-bricks up and using mud to seal them together.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: Heat Transportation - The Pump Module (PM) provides flow and accumulator functions and maintains proper temperature control at the pump outlet for each Loop. The PM consists of a single pump, a fixed charge accumulator, a Pump & Control Valve Package (PCVP) containing a firmware controller, startup heaters, isolation valves, and various sensors for monitoring performance. The Nitrogen Tank Assembly (NTA) controls the flow of ammonia out of the Ammonia Tank Assembly (ATA). The ATA contains two flexible, chambers incorporated into its ammonia tanks that expand as pressurized nitrogen from the NTA expels liquid ammonia out of the ATA. The major components in the ATA include two ammonia storage tanks, isolation valves, heaters, and various temperature, pressure, and quantity sensors.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The International Space Station (ISS) External Active Thermal Control System (EATCS)[1] maintains an equilibrium when the ISS environment or heat loads exceed the capabilities of the Passive Thermal Control System (PTCS). Note Elements of the PTCS are external surface materials, insulation such as Multi-Layer Insulation (MLI), or Heat Pipes. The EATCS provides heat rejection capabilities for all the U.S. pressurized modules, the Japanese Experiment Module (JEM), the Columbus Orbital Facility (COF), and the main power distribution electronics of the S0, S1 and P1 Trusses.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: Tranquility was built within the ESA-NASA ISS bartering system. ESA committed to build and fund both Harmony and Tranquility as well as the ATV in order to use NASA ISS facilities, fly astronauts on the Shuttle and for other ISS services. ESA teamed up with the Italian Space Agency (ASI) to manufacture both Harmony and Tranquility at Thales Alenia Space in Turin, Italy. The module pressure shell is constructed of 2219 aluminum and its debris shield is made from hardened 6061 aluminum. The metal is heat-treated, enabling it to have similar ballistics resistance to stainless steel.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The trajectory requires high launch energy, so the probe was launched on a Delta IV Heavy class launch vehicle and an upper stage based on the Star 48BV solid rocket motor.[30] Interplanetary gravity assists will provide further deceleration relative to its heliocentric orbit, which will result in a heliocentric speed record at perihelion.[4][35] As the probe passes around the Sun, it will achieve a velocity of up to 200 km/s (120 mi/s), which will temporarily make it the fastest human-made object, almost three times as fast as the previous record holder, Helios-2.[36][37][38] Like every object in an orbit, due to gravity the spacecraft will accelerate as it nears perihelion, then slow down again afterward until it reaches its aphelion.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The Sun is a G-type main-sequence star that constitutes about 99.86% of the mass of the Solar System. The Sun has an absolute magnitude of +4.83, estimated to be brighter than about 85% of the stars in the Milky Way, most of which are red dwarfs.[30][31] The Sun is a Population I, or heavy-element-rich,[b] star.[32] The formation of the Sun may have been triggered by shockwaves from one or more nearby supernovae.[33] This is suggested by a high abundance of heavy elements in the Solar System, such as gold and uranium, relative to the abundances of these elements in so-called Population II, heavy-element-poor, stars. The heavy elements could most plausibly have been produced by endothermic nuclear reactions during a supernova, or by transmutation through neutron absorption within a massive second-generation star.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The Sun's atmosphere is composed of four parts: the photosphere (visible under normal conditions), the chromosphere, the transition region, the corona and the heliosphere. During a total solar eclipse, the photosphere is blocked, making the corona visible.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The building uses extensively materials from Finnish nature, such as pine wood, copper, and natural rocks. Dipoli has 500 windows of which only four are identical. The architects originally planned for as little interference with the natural granite of the site as possible; but blasting the hard granite base rock inevitably fragmented it. The building is seen as a key example of organic architecture.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The Parker Solar Probe is the first spacecraft to fly into the low solar corona. It will assess the structure and dynamics of the Sun's coronal plasma and magnetic field, the energy flow that heats the solar corona and impels the solar wind, and the mechanisms that accelerate energetic particles. The spacecraft's systems are protected from the extreme heat and radiation near the Sun by a solar shield. Incident solar radiation at perihelion is approximately 650 kW/m2, or 475 times the intensity at Earth orbit.[1][30]: 31  The solar shield is hexagonal, mounted on the Sun-facing side of the spacecraft, 2.3 m (7 ft 7 in) in diameter,[31] 11.4 cm (4.5 in) thick, and is made of two panels of reinforced carbon–carbon composite with a lightweight 4.5-inch-thick carbon foam core,[32] which is designed to withstand temperatures outside the spacecraft of about 1,370 °C (2,500 °F).[1] The shield weighs only 73 kilograms (160 lb) and keeps the spacecraft's instruments at 29 °C (85 °F).
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: The radiative zone is the thickest layer of the sun, at 0.45 solar radii. From the core out to about 0.7 solar radii, thermal radiation is the primary means of energy transfer.[67] The temperature drops from approximately 7 million to 2 million Kelvin with increasing distance from the core.[55] This temperature gradient is less than the value of the adiabatic lapse rate and hence cannot drive convection, which explains why the transfer of energy through this zone is by radiation instead of thermal convection.[55] Ions of hydrogen and helium emit photons, which travel only a brief distance before being reabsorbed by other ions.[67] The density drops a hundredfold (from 20 g/cm3 to 0.2 g/cm3) between 0.25 solar radii and 0.7 radii, the top of the radiative zone.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: The Sun is the star at the center of the Solar System. It is a nearly perfect ball of hot plasma,[18][19] heated to incandescence by nuclear fusion reactions in its core. The Sun radiates this energy mainly as light, ultraviolet, and infrared radiation, and is the most important source of energy for life on Earth. The Sun's radius is about 695,000 kilometers (432,000 miles), or 109 times that of Earth. Its mass is about 330,000 times that of Earth, comprising about 99.86% of the total mass of the Solar System.[20] Roughly three-quarters of the Sun's mass consists of hydrogen (~73%); the rest is mostly helium (~25%), with much smaller quantities of heavier elements, including oxygen, carbon, neon, and iron.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: Earth is the third planet from the Sun and the only place known in the universe where life has originated and found habitability. While large volumes of water can be found throughout the Solar System, only Earth sustains liquid surface water. Approximately 70.8% of Earth's surface is made up of the ocean, dwarfing Earth's polar ice, lakes, and rivers. The remaining 29.2% of Earth's surface is land, consisting of continents and islands. Earth's surface layer is formed of several slowly moving tectonic plates, which interact to produce mountain ranges, volcanoes, and earthquakes. Earth's liquid outer core generates the magnetic field that shapes the magnetosphere of Earth, deflecting destructive solar winds.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: The Solar Maximum Mission satellite (or SolarMax) was designed to investigate Solar phenomena, particularly solar flares. It was launched on February 14, 1980. The SMM was the first satellite based on the Multimission Modular Spacecraft bus manufactured by Fairchild Industries, a platform which was later used for Landsats 4 and 5[1] as well as the Upper Atmosphere Research Satellite.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: Several new types of non-volatile RAM, which preserve data while powered down, are under development. The technologies used include carbon nanotubes and approaches utilizing Tunnel magnetoresistance. Amongst the 1st generation MRAM, a 128 kbit (128 × 210 bytes) chip was manufactured with 0.18 µm technology in the summer of 2003.[citation needed] In June 2004, Infineon Technologies unveiled a 16 MB (16 × 220 bytes) prototype again based on 0.18 µm technology. There are two 2nd generation techniques currently in development: thermal-assisted switching (TAS)[29] which is being developed by Crocus Technology, and spin-transfer torque (STT) on which Crocus, Hynix, IBM, and several other companies are working.[30] Nantero built a functioning carbon nanotube memory prototype 10 GB (10 × 230 bytes) array in 2004. Whether some of these technologies can eventually take significant market share from either DRAM, SRAM, or flash-memory technology, however, remains to be seen.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: The two widely used forms of modern RAM are static RAM (SRAM) and dynamic RAM (DRAM). In SRAM, a bit of data is stored using the state of a six-transistor memory cell, typically using six MOSFETs. This form of RAM is more expensive to produce, but is generally faster and requires less dynamic power than DRAM. In modern computers, SRAM is often used as cache memory for the CPU. DRAM stores a bit of data using a transistor and capacitor pair (typically a MOSFET and MOS capacitor, respectively),[27] which together comprise a DRAM cell. The capacitor holds a high or low charge (1 or 0, respectively), and the transistor acts as a switch that lets the control circuitry on the chip read the capacitor's state of charge or change it. As this form of memory is less expensive to produce than static RAM, it is the predominant form of computer memory used in modern computers.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: An MPLM is a large cylinder equipped with a common berthing mechanism at one end, and grapple fixtures to allow the Canadarm-2 to move it from the shuttle bay to a berthing port on the US Orbital Segment of the ISS.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: Each ISPR provides 1.571 m3 (55.5 ft3) of internal volume being about 2 m (79.3 in) high, 1.05 m (41.3 in) wide, and 85.9 cm (33.8 in) deep. The rack weighs 104 kg (230 lb) and can accommodate an additional 700 kg (1540 lb) of payload equipment.[1] The rack has internal mounting provisions to allow attachment of secondary structure. The ISPRs will be outfitted with a thin center post to accommodate sub-rack-sized payloads, such as the 483 mm (19-inch rack) Spacelab Standard Interface Rack (SIR) Drawer or the Space Shuttle Middeck Locker. Utility pass-through ports are located on each side to allow cables to be run between Racks. Module attachment points are provided at the top of the rack and via pivot points at the bottom. The pivot points support installation and maintenance. Tracks on the exterior front posts allow mounting of payload equipment and laptop computers. Additional adapters on the ISPRs are provided for ground handling.
  • Using base image: Yes

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

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  • Prompt: he HTV is about 9.8 metres (32 ft) long (including maneuvering thrusters at one end) and 4.4 metres (14 ft) in diameter. Total mass when empty is 10,500 kilograms (23,100 lb), with a maximum total payload of 6,000 kilograms (13,000 lb), for a maximum launch weight of 16,500 kilograms (36,400 lb).[2] The HTV is comparable in function to the Russian Progress, ESA ATV, commercial Cargo Dragon 1, and Cargo Dragon 2 of SpaceX. Plus the Cygnus spacecraft, all of which bring supplies to the ISS. Like the ATV, the HTV carries more than twice the payload of the Progress, but is launched less than half as often. Unlike Progress spacecraft, Cargo Dragon 2's and ATV's which use the docking ports automatically, HTVs and American Dragon 1 approach the ISS in stages, and once they reach their closest parking orbit to the ISS, crew grapple them using the robotic arm Canadarm2 and berth them to an open berthing port on the Harmony module.
  • Using base image: Yes