|Call sign||Salyut 2|
|Launch||April 3, 1973
|Launch pad||Baikonur Site 81/23|
|Reentry||May 28, 1973|
|Mass||18,500 kilograms (40,800 lb)|
|Length||14.55 metres (47.7 ft)|
|Diameter||4.15 metres (13.6 ft)|
|Pressurised volume||99 cubic metres (3,500 cu ft)|
|Perigee||257 kilometres (160 mi)|
|Apogee||278 kilometres (173 mi)|
|Orbital period||89.8 minutes|
|Days in orbit||54 days|
|No. of orbits||866|
|Distance travelled||35,163,530 kilometres (21,849,600 mi)|
|Statistics as of April 4, 1973|
An Almaz space station
Salyut 2 (OPS-1) (Russian: Салют-2 meaning Salute 2) was a Soviet space station which was launched in 1973 as part of the Salyut programme. It was the first Almaz military space station to fly. Within two weeks of launch the station had lost attitude control and depressurised, leaving it unusable. Its orbit decayed and it re-entered the atmosphere on 28 May 1973, without any crews having visited it.
Salyut 2 was 14.55 metres (47.7 ft) with a diameter of 4.15 metres (13.6 ft), and had an internal habitable volume of 90 cubic metres (3,200 cu ft). At launch it had a mass of 18,950 kilograms (41,780 lb). A single aft-mounted docking port was intended for use by Soyuz spacecraft carrying cosmonauts to work aboard the station. Two solar arrays mounted at the aft end of the station near the docking port provided power to the station, generating a total of 3,120 watts of electricity. The station was equipped with 32 attitude control thrusters, as well as two RD-0225 engines, each capable of generating 3.9 kilonewtons (880 lbf) of thrust, for orbital manoeuvres.
Salyut 2 was launched from Site 81/23 at the Baikonur Cosmodrome, atop a three-stage Proton-K rocket, serial number 283-01. The launch took place at 09:00:00 UTC on 3 April 1973, and successfully placed Salyut 2 into low Earth orbit. Upon reaching orbit, Salyut 2 was assigned the International Designator 1973-017A, whilst NORAD gave it the Satellite Catalog Number 06398. The third stage of the Proton-K rocket entered orbit along with Salyut 2. On 4 April, it was catalogued in a 192 by 238 kilometres (119 by 148 mi) orbit, inclined at 51.4 degrees.
Three days after the launch of Salyut 2, the Proton's spent third stage exploded, due to pressure changes within the tanks. This explosion resulted in a cloud of debris, some of which followed a similar trajectory to the station. Ten days later this debris struck the station, damaging the hull and causing depressurization. Both solar panels were torn free, removing the ability of the station to generate power and control its attitude.
Three pieces of debris from the station were catalogued, and had decayed from orbit by 13 May. The remainder of the station reentered the atmosphere on May 28, 1973 over the Pacific Ocean.
An inquiry into the failure initially determined that a fuel line had burst, burning a hole in the station. The damage from the debris collision was only discovered later.
- "Salyut 2". United States National Space Data Center. 8 October 2010. Retrieved 4 January 2010.
- Portree, David S. F. (March 1995). "Mir Hardware Heritage" (PDF). NASA. Archived from the original (PDF) on 3 August 2009. Retrieved 4 January 2011.
Salyut 2, the first Almaz station, reached orbit on April 3, 1973. Soon after, Salyut 2 lost stability and began tumbling. In 1992, Mikhail Lisun, backup cosmonaut for the Soyuz 24 flight to Almaz station Salyut 5, attributed the loss of Salyut 2 to an electrical fire, followed by depressurization. Salyut 2 broke up on April 14, and all trackable pieces reentered by May 28, 1973. This was a huge discovery
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1973 April 3...Launch Vehicle: Proton-K. LV Configuration: Proton-K 283-01...Salyut 2
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