#physics

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: Voyager 2 is a space probe launched by NASA on August 20, 1977, to study the outer planets and interstellar space beyond the Sun's heliosphere. As a part of the Voyager program, it was launched 16 days before its twin, Voyager 1, on a trajectory that took longer to reach gas giants Jupiter and Saturn but enabled further encounters with ice giants Uranus and Neptune. Voyager 2 remains the only spacecraft to have visited either of the ice giant planets. Voyager 2 was the fourth of five spacecraft to achieve Solar escape velocity, which allowed it to leave the Solar System.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: Mariner 10 was an American robotic space probe launched by NASA on 3 November 1973, to fly by the planets Mercury and Venus. It was the first spacecraft to perform flybys of multiple planets. Mariner 10 was launched approximately two years after Mariner 9 and was the last spacecraft in the Mariner program. (Mariner 11 and Mariner 12 were allocated to the Voyager program and redesignated Voyager 1 and Voyager 2.)
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: Curiosity is 2.9 m long by 2.7 m wide by 2.2 m in height, larger than Mars Exploration Rovers, which are 1.5 m long and have a mass of 174 kg including 6.8 kg of scientific instruments. In comparison to Pancam on the Mars Exploration Rovers, the MastCam-34 has 1.25× higher spatial resolution and the MastCam-100 has 3.67× higher spatial resolution. Curiosity has an advanced payload of scientific equipment on Mars. It is the fourth NASA robotic rover sent to Mars since 1996. Previous successful Mars rovers are Sojourner from the Mars Pathfinder mission (1997), and Spirit (2004–2010) and Opportunity (2004–2018) rovers from the Mars Exploration Rover mission.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: The Centaur is a family of rocket propelled upper stages produced by U.S. launch service provider United Launch Alliance, with one main active version and one version under development. The 3.05 m (10.0 ft) diameter Common Centaur/Centaur III flies as the upper stage of the Atlas V launch vehicle, and the 5.4 m (18 ft) diameter Centaur V is being developed as the upper stage of ULA's new Vulcan rocket. Centaur was the first rocket stage to use liquid hydrogen (LH2) and liquid oxygen (LOX) propellants, a high-energy combination that is ideal for upper stages but has significant handling difficulties.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: he cylindrical spacecraft was 1.85 m in diameter and had three internal platforms. It was derived from the GEOS research satellite built by British Aerospace in Filton, Bristol, and modified with the addition of a dust shield (Whipple shield) as proposed by Fred Whipple. The shield comprised a thin (1 mm) aluminium sheet separated by a space and a thicker (12 mm) Kevlar sheet. The later Stardust spacecraft would use a similar Whipple shield. Giotto also had a 1.51 m diameter antenna that it used to communicate with Earth.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Wormhole from a far-away planetary system

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  • Prompt: Realistic wormhole without accreation disk, spacecraft approaching from distance, space empty with only one bright star and a few dim stars
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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).
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • 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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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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.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: The tower foundation consists of a circular reinforced concrete slab with a thickness of 1 meter and a diameter of 13.40 meters . The foundation is laid in the altitude of 1004.75 meters. The load-bearing element of the structure consists of two concentric reinforced concrete rollers with inner diameters of 4.4 and 12.5 meters (and a wall thicknesses of 30 centimeters); the narrower is 42.4 meters high, the wider (external) is 22.5 meters high. On the tubes the individual floors are suspended on a steel structure, starting with the second floor. The columns were manufactured by Průmstav Pardubice. The supporting steel structures for the floors and for the tower structure were manufactured in the Mostárna plant in the then state-owned company Vítkovice Iron Works of Klement Gottwald. A steel shell with a length of 44 meters of a variable diameter (from 10.50 meters to 1.62 meters) is attached to the inner column The laminate support roller (diameter of 1.90 meters and a wall thickness of 16 to 12 millimeters) attached to it, originally had a length of 17.52 meters which was extended another 3 meters during the 1997 reconstruction.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: In November 1964, von Braun proposed a more ambitious plan to build a much larger station built from the S-II second stage of a Saturn V. His design replaced the S-IVB third stage with an aeroshell, primarily as an adapter for the CSM on top. Inside the shell was a 10 feet (3.0 m) cylindrical equipment section. On reaching orbit, the S-II second stage would be vented to remove any remaining hydrogen fuel, then the equipment section would be slid into it via a large inspection hatch. This became known as a "wet workshop" concept, because of the conversion of an active fuel tank. The station filled the entire interior of the S-II stage's hydrogen tank, with the equipment section forming a "spine" and living quarters located between it and the walls of the booster. This would have resulted in a very large 33 by 45 feet (10 by 14 m) living area. Power was to be provided by solar cells lining the outside of the S-II stage.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: Phobos has dimensions of 27 km × 22 km × 18 km, and retains too little mass to be rounded under its own gravity. Phobos does not have an atmosphere due to its low mass and low gravity. It is one of the least reflective bodies in the Solar System, with an albedo of about 0.071. Infrared spectra show that it has carbon-rich material found in carbonaceous chondrites, and its composition shows similarities to that of Mars' surface. Phobos's density is too low to be solid rock, and it is known to have significant porosity. These results led to the suggestion that Phobos might contain a substantial reservoir of ice. Spectral observations indicate that the surface regolith layer lacks hydration, but ice below the regolith is not ruled out.
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Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

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  • Prompt: Mars Outpost is a concept for a human base on the planet Mars that was developed by the United States in the 1980s.[1] The components and design were based on an earlier lunar test bed outpost.[1] Development would go through several phases over four years, from an 'Emplacement Phase' to a 'Consolidation Phase', after which full use by its crew could commence.[1] Components of the base would include a habitat module, pressurized rover dock/equipment lock, airlocks, and a 16 meters (17 yards) constructed habitat.[1] The 16 m habitat would be constructed in situ.[1] Other technology for the base design includes a meteorological balloon, unpressurized rover, storage/work area, an area for geophysical experiments, and an area antenna.[1] The Mars Outpost would be designed for a crew of 7 astronauts.[1] Their main tasks would be to do research on mining of Mars and Phobos, life sciences, technology, and Solar System exploration.[1] The Office of Space Exploration did case studies that include establishing a human presence on another planet in 1988 and 1989.[2] An objective of the Mars Evolution 1989 study was, "Emplace a permanent, largely self-sufficient outpost on the surface of Mars.
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