Module 1 -Zarya
Zarya , also known as the Functional Cargo Block or the FGB was the first module of the International Space Station to be launched. The FGB provided electrical power, storage, propulsion, and guidance to the ISS during the initial stage of assembly. As other modules with more specialized functionality are constructed, the Zarya's role will primarily be storage, both inside the pressurized section and in the externally mounted fuel tanks. The Zarya is a descendant of the TKS spacecraft designed for the Russian Salyut program. The name "Zarya", meaning "Dawn" in Russian, was given to the FGB because it signified the dawn of a new era of international cooperation in space.
Construction
It is owned and paid for by the United States and was built from December 1994 to January 1998 in Russia in the Khrunichev State Research and Production Space Center (KhSC) in Moscow. It was included as part of the plan instead of Lockheed's 'Bus-1' option because it would be significantly cheaper ($220 million vs. $450 million). As part of the contract Khrunichev constructed most of an identical module (referred to as "FGB-2") for contingency purposes. This has been proposed for a variety of projects, including a potential replacement for Progress spacecraft, the Docking and Storage module, the Universal Docking module, a commercial space module, or an independent space station.
Design
Zarya weighs 19,300 kg (42,600 pounds), is 12.55 m (41.2 feet) long and 4.1 m (13.5 feet) wide at its widest point.Zarya has three docking ports, one on each end, and one on the side. Zvezda is attached to the aft port, the Pressurized Mating Adapter attached to the forward port connects to the Unity Module, and the side (axial or nadir) port is used to dock with either a Russian Soyuz or a Progress spacecraft, until the Docking Cargo Module is docked there permanently. Zarya has two solar arrays, measuring 10.67 m by 3.35 m, and six nickel-cadmium batteries that can provide on average 3 kilowatts of power. Zarya has 16 external fuel tanks that can hold over 6 metric tons of propellant, with 24 large steering jets, 12 small steering jets, and two large engines for reboost and major orbital changes.
It is owned and paid for by the United States and was built from December 1994 to January 1998 in Russia in the Khrunichev State Research and Production Space Center (KhSC) in Moscow. It was included as part of the plan instead of Lockheed's 'Bus-1' option because it would be significantly cheaper ($220 million vs. $450 million). As part of the contract Khrunichev constructed most of an identical module (referred to as "FGB-2") for contingency purposes. This has been proposed for a variety of projects, including a potential replacement for Progress spacecraft, the Docking and Storage module, the Universal Docking module, a commercial space module, or an independent space station.
Design
Zarya weighs 19,300 kg (42,600 pounds), is 12.55 m (41.2 feet) long and 4.1 m (13.5 feet) wide at its widest point.Zarya has three docking ports, one on each end, and one on the side. Zvezda is attached to the aft port, the Pressurized Mating Adapter attached to the forward port connects to the Unity Module, and the side (axial or nadir) port is used to dock with either a Russian Soyuz or a Progress spacecraft, until the Docking Cargo Module is docked there permanently. Zarya has two solar arrays, measuring 10.67 m by 3.35 m, and six nickel-cadmium batteries that can provide on average 3 kilowatts of power. Zarya has 16 external fuel tanks that can hold over 6 metric tons of propellant, with 24 large steering jets, 12 small steering jets, and two large engines for reboost and major orbital changes.
Specifications
Length: 12.56 m
Diameter: 4.11 m
Solar array length: 10.67 m
Solar array width: 3.35 m
Mass: 42,600 lb (19,300 kg)
Launch of Zarya module
