Russian manned spacecraft module. Operational, first launch 1989.08.23 (Progress M-1). Fuel module for refueling space stations. Refuelling section.
AKA: Otsek komponentov dozapravki.
Gross mass: 1,980 kg (4,360 lb).
Payload: 1,200 kg (2,600 lb).
Height: 2.24 m (7.34 ft).
Diameter: 2.17 m (7.11 ft).
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Associated Countries
Associated Spacecraft
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Progress M Russian logistics spacecraft. Operational, first launch 1989.08.23 (Progress M-1). Progress M was an upgraded version of the original Progress. New service module and rendezvous and docking systems were adopted from Soyuz T. More...
See also
Associated Propellants
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H2O2 Hydrogen peroxide is used as both an oxidiser and a monopropellant. Relatively high density and non-toxic, it was abandoned after early use in British rockets, but recently revived as a propellant for the Black Horse spaceplane. Hydrogen peroxide is used as both an oxidiser and a monopropellant. Relatively high density and non-toxic, it was abandoned after early use in British rockets, but recently revived as a propellant for the Black Horse spaceplane. More...
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