![]() Memorial to victims of the disaster | |
Date | 19:01 MSK (16:01 GMT) 18 March 1980 |
---|---|
Location | Plesetsk Cosmodrome Site 43 |
Casualties | |
48 dead [lower-alpha 1] | |
87 injured (43 seriously) |
The 1980 Plesetsk launch pad disaster was the explosion of a Vostok-2M rocket carrying a Tselina-D satellite during fueling at Site 43 of the Plesetsk Cosmodrome in Mirny at 19:01 local time (16:01 GMT) on 18 March 1980, two hours and fifteen minutes before the intended launch time. Forty-four people were killed in the initial fire and four more soon died in the hospital from burns. It is the second deadliest space exploration related disaster in history.
On 17 March the rocket was installed at the launch site. Various preliminary tests conducted before the fueling went as expected and without problem. The launch of the rocket was scheduled to take place at 21:16 on 18 March. Several hours before the intended launch, the tanks were filled with kerosene at 19:00 and preceded by the addition of liquid oxygen and liquid nitrogen to side tanks. After the addition of hydrogen peroxide was completed, a huge explosion at the site was witnessed at 19:01 MSK; 44 people in the area were killed instantly and another 43 required hospitalization for burns, four of whom later died while in the hospital. Many of the survivors suffered severe burns and lung damage. Over 80% of surviving eyewitnesses to the disaster reported that the first explosion originated from Block E of the rocket and was followed by multiple secondary explosions. The 300 tons of fuel destroyed the launch pad and surrounding area. [1] [2]
The official investigation responsible for determining the cause of the disaster headed by Leonid Smirnov assigned blame to the crew that was killed at the site of the fire by specifically stating the official cause as "explosion (inflammation) of material soaked in liquid oxygen as a result of unauthorized actions of one of the members of the ground crew". However, less than a year later, on 23 July 1981 after a second disaster of the same cause was narrowly avoided, it was discovered that a design flaw in the fuel filters of the rocket were likely the cause of the 1980 disaster, although it was impossible to confirm which type of filters were used in the rocket that exploded. The catalytically active lead solder on the filters would cause an explosion upon contact with hydrogen peroxide. [1] [3] [4]
The disaster was not reported in Soviet media at the time and only reached western media outlets in 1989 upon declassification. Pravda reported that the launch of the rocket was a success and did not say anything about the explosion. [5] [6] [7]
A hybrid-propellant rocket is a rocket with a rocket motor that uses rocket propellants in two different phases: one solid and the other either gas or liquid. The hybrid rocket concept can be traced back to the early 1930s.
The Baikonur Cosmodrome is a spaceport operated by Russia within Kazakhstan. Located in the Kazakh city of Baikonur, it is the largest operational space launch facility in terms of area. All Russian crewed spaceflights are launched from Baikonur.
Plesetsk Cosmodrome is a Russian spaceport located in Mirny, Arkhangelsk Oblast, about 800 km north of Moscow and approximately 200 km south of Arkhangelsk. As of 2024, it is Europe's only operational orbital spaceport and the northernmost spaceport in the world. Originally developed as an ICBM site for the R-7 missile, it also served for numerous satellite launches using the R-7 and other rockets. Its high latitude makes it useful only for certain types of launches, especially the Molniya orbits, so for much of the site's history it functioned as a secondary location, with most orbital launches taking place from Baikonur, in the Kazakh SSR. With the end of the Soviet Union, Baikonur became a foreign territory, and Kazakhstan charged $115 million usage fees annually. Consequently, Plesetsk has seen considerably more activity since the 2000s.
A launch pad is an above-ground facility from which a rocket-powered missile or space vehicle is vertically launched. The term launch pad can be used to describe just the central launch platform, or the entire complex. The entire complex will include a launch mount or launch platform to physically support the vehicle, a service structure with umbilicals, and the infrastructure required to provide propellants, cryogenic fluids, electrical power, communications, telemetry, rocket assembly, payload processing, storage facilities for propellants and gases, equipment, access roads, and drainage.
The Nedelin catastrophe or Nedelin disaster, known in Russia as the Catastrophe at Baikonur Cosmodrome, was a launch pad accident that occurred on 24 October 1960 at the Baikonur Cosmodrome in Soviet Kazakhstan. As a prototype of the R-16 intercontinental ballistic missile was being prepared for a test flight, an explosion occurred when the second stage engine ignited accidentally, killing an unknown number of military and technical personnel working on the preparations. Despite the magnitude of the disaster, information was suppressed for many years and the Soviet government did not acknowledge the event until 1989. With more than 54 casualties, it is the deadliest disaster in space exploration history. The catastrophe is named for the Chief Marshal of Artillery Mitrofan Ivanovich Nedelin, who was the head of the R-16 development program and perished in the explosion.
Vostok was a family of rockets derived from the Soviet R-7 Semyorka ICBM and was designed for the human spaceflight programme. This family of rockets launched the first artificial satellite and the first crewed spacecraft (Vostok) in human history. It was a subset of the R-7 family of rockets.
A liquid-propellant rocket or liquid rocket utilizes a rocket engine burning liquid propellants. (Alternate approaches use gaseous or solid propellants.) Liquids are desirable propellants because they have reasonably high density and their combustion products have high specific impulse (Isp). This allows the volume of the propellant tanks to be relatively low.
Korabl-Sputnik 3 or Vostok-1K No.3, also known as Sputnik 6 in the West, was a Soviet spacecraft which was launched in 1960. It was a test flight of the Vostok spacecraft, carrying two dogs; Pcholka and Mushka, as well as a television camera and scientific instruments.
The Angara rocket family is a family of launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The launch vehicles are to put between 3,800 kg (8,400 lb) and 24,500 kg (54,000 lb) into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles.
The highest specific impulse chemical rockets use liquid propellants. They can consist of a single chemical or a mix of two chemicals, called bipropellants. Bipropellants can further be divided into two categories; hypergolic propellants, which ignite when the fuel and oxidizer make contact, and non-hypergolic propellants which require an ignition source.
The Meteor spacecraft are weather observation satellites launched by the Soviet Union and Russia. The Meteor satellite series was initially developed during the 1960s. The Meteor satellites were designed to monitor atmospheric and sea-surface temperatures, humidity, radiation, sea ice conditions, snow-cover, and clouds. Between 1964 and 1969, a total of eleven Soviet Union Meteor satellites were launched.
The Zenit-2 was a Ukrainian, previously Soviet, expendable carrier rocket. First flown in 1985, it has been launched 37 times, with 6 failures. It is a member of the Zenit family of rockets and was designed by the Yuzhmash.
The R-7 family of rockets is a series of rockets, derived from the Soviet R-7 Semyorka, the world's first intercontinental ballistic missile (ICBM). More R-7 rockets have been launched than any other family of large rockets.
Site 133, also known as Raduga, is a launch complex at the Plesetsk Cosmodrome in Russia. It is used by Rockot, and previously Kosmos carrier rockets. It consists of a single pad, originally designated 133/1, and later 133/3.
Site 43, also known as SK-3 and SK-4, is a launch complex at the Plesetsk Cosmodrome in Russia. It consists of a two pads, Sites 43/3 and 43/4, and has been used by R-7 derived rockets since the early 1960s.
The Soyuz-2.1v, GRAU index 14A15, known earlier in development as the Soyuz-1, is a Russian expendable launch vehicle. It is a heavily modified derivative of the Soyuz-2.1b, and is a member of the R-7 family of rockets. It is built by TsSKB Progress, at Samara in Russia. Launches are conducted from existing facilities at the Plesetsk Cosmodrome in Northwest Russia, with pads also available at the Baikonur Cosmodrome in Kazakhstan, and new facilities at the Vostochny Cosmodrome in Eastern Russia.
The Vostok-2, GRAU index 8A92 was an expendable carrier rocket used by the Soviet Union between 1962 and 1967. Forty five were launched, of which five failed. It was derived from the earlier Vostok-K, with uprated engines. It was a member of the Vostok family of rockets.
The Vostok-2M, GRAU index 8A92M was an expendable carrier rocket used by the Soviet Union between 1964 and 1991. Ninety-three were launched, of which one failed. Another was destroyed before launch. It was originally built as a specialised version of the earlier Vostok-2, for injecting lighter payloads into higher Sun-synchronous orbits. It was a member of the R-7 family of rockets, and the last Vostok.
Kosmos 112 or Zenit-2 No.36 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 112 was the thirty-sixth of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb). It was the first satellite to be launched from the Plesetsk Cosmodrome.