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Almaz APOS
Part of Almaz

Almaz

Almaz
Forward view of Almaz space station - original configuration. From left to right note stowed solar panels, sunshade for Agat reconnaissance camera extending below first station compartment, VA re-entry capsule and its launch escape rocket.
Credit: © Dietrich Haeseler

Russian manned space station. Cancelled 1966. The initial Almaz phase 1 configuration as conceived in 1965 included a single-launch station with its own VA crew return re-entry module.

AKA: 11F71+111F74;APOS. Status: Cancelled 1966. Thrust: 7.84 kN (1,763 lbf). Gross mass: 19,900 kg (43,800 lb). Specific impulse: 291 s.

In the 1970's plans for launch of an Almaz equipped with a VA would be renewed - but at the expense of most of the station's sensor payload, which would be delivered by TKS ferries.

Crew Size: 3. Spacecraft delta v: 100 m/s (320 ft/sec).



Family: Space station, Space station orbit. Country: Russia. Engines: RD-0225. Launch Vehicles: Proton, Proton-K. Propellants: N2O4/UDMH. Agency: Chelomei bureau, MOM. Bibliography: 376, 443, 474.
Photo Gallery

Almaz 1965Almaz 1965


Almaz forward viewAlmaz forward view
Forward view of Almaz space station - original configuration, Note crew couches in cutaway view of VA re-entry capsule interior. The Almaz was actually flown without the VA. Also note the orientation engines just below the VA attachment collar.
Credit: © Dietrich Haeseler


Rear view of AlmazRear view of Almaz
Rear view of Almaz model. Note the two manoeuvring engines flanking the docking collar, the stowed solar panels, and the guides for aft interstage separation
Credit: © Dietrich Haeseler


Almaz interiorAlmaz interior
Close-up view of interior of Almaz space station. Note large white film cassettes of reconnaissance camera, and cosmonaut at the control station of the camera systems.
Credit: © Dietrich Haeseler


Almaz OriginalAlmaz Original
Almaz - Early configuration with VA return capsule.
Credit: © Reginaldo Miranda Jr



1964 February 15 - .
1964 October 12 - . LV Family: Proton. Launch Vehicle: Proton-K.
1965 January 1 - .

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