Almaz APOS (original) (raw)


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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 1965 Almaz 1965


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


Almaz interior Almaz interiorClose-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 Original Almaz OriginalAlmaz - 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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