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International Space Station solar array wing (Expedition 17 crew, August 2008).An ISS solar panel intersecting Earth's horizon.. The electrical system of the International Space Station is a critical part of the International Space Station (ISS) as it allows the operation of essential life-support systems, safe operation of the station, operation of science equipment, as well as improving crew ...
Zvezda provided early living quarters, a life support system, a communication system (Zvezda introduced a 10 Mbit/s Ethernet network to the ISS [31]), electrical power distribution, a data processing system, a flight control system, and a propulsion system. These quarters and some, but not all, systems have since been supplemented by additional ...
On 26 October 2007, the station's Space Station Remote Manipulator System (SSRMS) removed Harmony from the shuttle cargo bay and temporarily mated it to the port side of Unity and, on 27 October 2007, the crew entered in Harmony. [6] [26] After the Space Shuttle departed, Harmony was relocated to the forward dock of the Destiny laboratory.
The electrical connections are compatible with the Space Station Remote Manipulator System (also known as Canadarm2). It is used on the International Space Station (ISS). PDGFs can be "grappled" by the Canadarm2 robotic arm, in order to allow the arm to manipulate and power a grappled object, or be commanded by operators based inside the ISS.
The EATCS is capable of rejecting up to 70 kW, and provides a substantial upgrade in heat rejection capacity from the 14 kW capability of the Early External Active Thermal Control System (EEATCS) via the Early Ammonia Servicer (EAS), which was launched on STS-105 and installed onto the P6 Truss. [1]
Russian components of the International Space Station (16 P) Pages in category "Components of the International Space Station" The following 48 pages are in this category, out of 48 total.
ISS Propulsion Module (NASA) The ISS Propulsion module was proposed as a backup to functions performed by the Zvezda Service Module and Progress spacecraft.Critical ISS functionality such as guidance, navigation, control and propulsion are provided only by Russian (Zvezda and Progress) and the European spacecraft. [1]
Its origins lie in designs for the Pressurized Docking Mast, [1] consisting of an off-axis frustoconical docking tunnel contained within a framework and a retractable coupling mechanism, later part of the Pressurized Berthing Adapter assembly that appeared in designs for Space Station Freedom 1987, and the reduced design referred to as 'Fred' [2] 1991.