משתמש:Cgruda/ארג"ח4 – הבדלי גרסאות
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שורה 97:
===הרכבה===
===יחידות מדוחסות===
{| class="wikitable" style="width:auto; margin:auto;"
|- style="background:#EFEFEF;"
! מודול
! משלחת
! שיגור
! משגר
! style="width:100px;"| מדינה
! style="width:82px;"| מראה
! style="width:82px;"| מראה בתחנה
|-
| rowspan="2" | [[יחידת הליבה של מיר]]<br/><small>(יחידת הליבה)</small>
| N/A
| [[19 בפברואר]] [[1986]]
| [[פרוטון (משגר לוויינים)|פרוטון K]]
| [[בריה"מ]]
| rowspan="2" | [[File:RP1357 p103 Mir base block.svg|80px|upright| alt=A line diagram of a DOS spacecraft. The module consists of a stepped cylinder, with two large solar arrays projecting from opposing sides of the narrower portion of the module. A spherical compartment with five docking ports is attached to the end of the narrower section, whilst a lollipop-shaped antenna projects radially from the far end of the wider section.]]
| rowspan="2" | <center>[[File:Mir Core Module.JPG|40px| alt=A photograph of a DOS spacecraft. The module consists of a stepped cylinder, with two large solar arrays projecting from opposing sides of the narrower portion of the module. A spherical compartment with five docking ports is attached to the end of the narrower section, whilst a lollipop-shaped antenna projects radially from the far end of the wider section.]]</center>
|- style="border-bottom: 3px solid gray"
| colspan="4" | The base block for the entire ''Mir'' complex, the core module, or DOS-7, provided the main living quarters for resident crews and contained environmental systems, early attitude<!--It's supposed to be ATTitude, meaning orientation - please don't change this to aLTitude.--> control systems and the station's main engines. The module was based on hardware developed as part of the [[Salyut program]]me, and consisted of a stepped-cylinder main compartment and a spherical 'node' module, which served as an airlock and provided ports to which four of the station's expansion modules were berthed and to which a Soyuz or Progress spacecraft could dock. The module's aft port served as the berthing location for [[Kvant-1|''Kvant''-1]].<ref name="MHH">{{cite book|url=http://en.wikisource.org/wiki/Mir_Hardware_Heritage|title=Mir Hardware Heritage|author=David S. F. Portree|publisher=NASA|date=March 1995}}</ref>
|-
| rowspan="2" | [[Kvant-1|''Kvant''-1]]<br/><small>(Astrophysics Module)</small>
| [[Mir EO-2|EO-2]]
| 31 March 1987
| [[Proton-K]]
| Soviet Union
| rowspan="2" | [[File:RP1357 p162 Kvant module.svg|80px| alt=A line diagram of a short, cylindrical Kvant space station module, with a docking port in the centre of the visible circular face. A more angular section is visible behind the cylinder, and various antennas project from the module.]]
| rowspan="2" | [[File:Mir-kvant.jpg|80px| alt=An image of a white insulation covered, stepped-cylindrical module with a number of docking ports visible on a sphere at one end and three solar arrays projecting from the narrower portion of the stepped cylinder. A second, shorter module covered in darker insulation is docked to the end opposite that of the sphere, and a Soyuz spacecraft is docked to the other end of this module. The blackness of space serves as the image backdrop.]]
|- style="border-bottom: 3px solid gray"
| colspan="4" | The first expansion module to be launched, ''Kvant''-1 consisted of two pressurised working compartments and one unpressurised experiment compartment. Scientific equipment included an [[X-ray telescope]], an [[Ultraviolet astronomy|ultraviolet telescope]], a wide-angle camera, high-energy X-ray experiments, an X-ray/gamma ray detector, and the Svetlana electrophoresis unit. The module also carried six [[Gyroscope|gyrodynes]] for attitude<!--It's supposed to be ATTitude, meaning orientation - please don't change this to aLTitude.--> control, in addition to life support systems including an [[Elektron (ISS)|Elektron]] oxygen generator and a [[Vozdukh]] carbon dioxide remover.<ref name="MHH"/>
|-
| rowspan="2" | [[Kvant-2|''Kvant''-2]]<br/><small>(Augmentation Module)</small>
| [[Mir EO-5|EO-5]]
| 26 November 1989
| [[Proton-K]]
| Soviet Union
| rowspan="2" | [[File:RP1357 p164 Kvant 2 module.svg|80px| alt=A line diagram of a Kvant 2 space station module, consisting of a stepped-cylindrical shape. Two large solar arrays project from the centre of the module on the wider section, and a cone-shaped airlock is seen at the distal end of the narrower section. Various spherical pieces of equipment and antennas project from the module.]]
| rowspan="2" | [[File:Mir Kvant 1-Base Block-Kvant 2.jpg|80px| alt=Three space station modules, connected in a supine L-shape. At the left is a Soyuz spacecraft docked to a short, stubby module, in turn docked to a larger, stepped-cylindrical module covered in white insulation, from which solar arrays project. To that module is attached a third module, similar in size, at a right angle, forming the short stroke of the L. This module is also projecting two hard-to-see solar arrays. The cloudy Earth is the backdrop.]]
|- style="border-bottom: 3px solid gray"
| colspan="4" | The first [[TKS spacecraft|TKS]] based module, ''Kvant''-2, was divided into three compartments; an [[Extra-vehicular activity|EVA]] airlock, an instrument/cargo compartment (which could function as a backup airlock), and an instrument/experiment compartment. The module also carried a Soviet version of the [[Manned Maneuvering Unit]] for the [[Orlan space suit]], referred to as [[Astronaut Propulsion Unit#Soviet SPK|''Ikar'']], a system for regenerating water from urine, a shower, the ''Rodnik'' water storage system and six [[gyroscopes|gyrodynes]] to augment those already located in ''Kvant''-1. Scientific equipment included a high-resolution camera, spectrometers, X-ray sensors, the Volna 2 fluid flow experiment, and the Inkubator-2 unit, which was used for hatching and raising [[quail]].<ref name="MHH"/>
|-
| rowspan="2" | ''[[Kristall]]''<br/><small>(Technology Module)</small>
| [[Mir EO-6|EO-6]]
| 31 May 1990
| [[Proton-K]]
| Soviet Union
| rowspan="2" | [[File:RP1357 p166 Kristall module.svg|80px| alt=A line diagram of a space station module, consisting of a narrow cylinder with a sphere attached to the distal end. The sphere features two docking ports, one on the distal face and another on one of the lateral faces, and two concertinaed solar arrays project from the module. Various spherical pieces of equipment and antennas are mounted to the module.]]
| rowspan="2" | [[File:Mir from Soyuz TM-17.jpg|80px| alt=An image of a space station consisting of four modules arranged in a T-shape. A short, stubby module is docked to a longer, stepped-cylindrical module which has a number of docking ports arranged in a sphere at one end. Two other modules, similar in size, project from opposing ports on this sphere. A Progress spacecraft is docked to the short module, a Soyuz spacecraft to the end of the lower module in the crossbar of the T, and another Progress spacecraft is seen a distance away from the module cluster, carrying out undocking operations.]]
|- style="border-bottom: 3px solid gray"
| colspan="4" | ''Kristall'', the fourth module, consisted of two main sections. The first was largely used for materials processing (via various processing furnaces), astronomical observations, and a biotechnology experiment utilising the Aniur electrophoresis unit. The second section was a docking compartment which featured two [[APAS-89]] [[Spacecraft docking|docking ports]] initially intended for use with the [[Buran (spacecraft)|''Buran'']] [[Buran program|programme]] and eventually used during the [[Shuttle-Mir Program|Shuttle-''Mir'' programme]]. The docking compartment also contained the Priroda 5 camera used for Earth resources experiments. ''Kristall'' also carried six [[Gyroscope|gyrodine]]s for attitude<!--It's supposed to be ATTitude, meaning orientation - please don't change this to aLTitude.--> control to augment those already on the station, and two collapsible solar arrays.<ref name="MHH"/>
|-
| rowspan="2" | ''[[Spektr]]''<br/><small>(Power Module)</small>
| [[Mir EO-18|EO-18]]
| 20 May 1995
| [[Proton-K]]
| Russia
| rowspan="2" | [[File:Spektr module drawing.png|80px| alt=A line diagram of a space station module consisting of a large cylinder with a shallow cone at one end and a steeper cone at the other. The shallow cone has a docking port mounted in the centre, while the steeper cone has two large solar arrays projecting from it. Two more arrays are mounted at the base of the cone.]]
| rowspan="2" | [[File:Mir from STS-74.jpg|80px| alt=A space station consisting of three white modules arranged in a T shape around a central docking node. A fifth module projects upward from the docking node, with a sixth module attached to its end. A Progress and Soyuz spacecraft are docked to the station, and each of the modules projects various feathery solar arrays, antennas and trusses. The blackness of space forms the backdrop to the image.]]
|- style="border-bottom: 3px solid gray"
| colspan="4" | ''Spektr'' was the first of the three modules launched during the Shuttle-''Mir'' programme; it served as the living quarters for American astronauts and housed NASA-sponsored experiments. The module was designed for remote observation of Earth's environment and contained atmospheric and surface research equipment. Additionally, it featured four solar arrays which generated approximately half of the station's electrical power. The module also featured a science airlock to expose experiments to the vacuum of space selectively. ''Spektr'' was rendered unusable following the collision with [[Progress M-34]] in 1997 which damaged the module, exposing it directly to the vacuum of space.<ref name="SSSM"/>
|-
| rowspan="2" | [[Mir Docking Module|Docking Module]]
| [[Mir EO-20|EO-20]]
| 15 November 1995
| {{OV|104}}<br>([[STS-74]])
| US
| rowspan="2" | [[File:Mir Docking Module drawing.svg|80px| alt=A line diagram of a small, cylindrical space station module with a docking port on either end and two cuboid boxes mounted to its upper surface.]]
| rowspan="2" | [[File:Mir from STS-74PLB.jpg|80px| alt=A space station consisting of three white modules arranged in a T shape around a central docking node. The module on the downstroke of the T has a smaller, orange module attached to the distal end of it, and a fifth module projects rearward from the docking node, with a sixth module attached to its end. A Progress and Soyuz spacecraft are docked to the station, and each of the modules projects various feathery solar arrays, antennas and trusses. The blackness of space forms the backdrop to the image, and the sills of a space shuttle's payload bay can be seen at the bottom of the image.]]
|- style="border-bottom: 3px solid gray"
| colspan="4" | The docking module was designed to help simplify [[Space Shuttle]] [[Spacecraft docking|dockings]] to ''Mir''. Before the first shuttle docking mission ([[STS-71]]), the ''[[Kristall]]'' module had to be tediously moved to ensure sufficient clearance between ''Atlantis'' and ''Mir'''s solar arrays. With the addition of the docking module, enough clearance was provided without the need to relocate ''Kristall''. It had two identical [[APAS-89]] docking ports, one attached to the distal port of ''Kristall'' with the other available for shuttle docking.<ref name="SSSM"/>
|-
| rowspan="2" | ''[[Priroda]]''<br/><small>(Earth Sensing Module)</small>
| [[Mir EO-21|EO-21]]
| 26 April 1996
| [[Proton-K]]
| Russia
| rowspan="2" | [[File:Priroda module drawing.svg|80px| alt=A line diagram of a Priroda space station module consisting of a large cylinder with a shallow cone, featuring a docking port, mounted to one end. A large dish-shaped antenna is mounted to the side of the cylinder.]]
| rowspan="2" | [[File:Mir from STS-81.jpg|80px| alt=An image of the Mir space station consisting of four modules (the rightmost one with a smaller orange module attached to its distal end) arranged in a cross shape about a central docking node. A sixth module projects rearward from this node, and has a seventh, smaller module attached to the far end. A Soyuz spacecraft is docked at the end of this stack. Each of the modules is projecting various feathery solar arrays, antennas and trusses, and the blackness of space forms the backdrop to the image.]]
|- style="border-bottom: 3px solid gray"
| colspan="4" | The seventh and final ''Mir'' module, ''Priroda'''s primary purpose was to conduct Earth resource experiments through remote sensing and to develop and verify remote sensing methods. The module's experiments were provided by twelve different nations, and covered microwave, visible, near infrared, and infrared spectral regions using both passive and active sounding methods. The module possessed both pressurised and unpressurised segments, and featured a large, externally mounted [[synthetic aperture radar]] dish.<ref name="SSSM"/>
|}
==הערות שוליים==
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