Mission type | Venus flyby [1] |
---|---|
Operator | OKB-1 |
COSPAR ID | 1965-094A |
SATCAT no. | 01742 |
Mission duration | 16 days |
Spacecraft properties | |
Spacecraft type | 3MV-4 |
Manufacturer | OKB-1 |
Launch mass | 6510 kg [2] |
Dry mass | 960 kg |
Start of mission | |
Launch date | 23 November 1965 03:22:00 GMT |
Rocket | Molniya 8K78 s/n U15000-30 [3] |
Launch site | Baikonur, Site 31/6 |
Contractor | OKB-1 |
End of mission | |
Disposal | Launch failure |
Decay date | 9 December 1965 |
Orbital parameters | |
Reference system | Geocentric [4] |
Regime | Low Earth |
Perigee altitude | 227 km |
Apogee altitude | 310 km |
Inclination | 51.9° |
Period | 89.8 minutes |
Epoch | 23 November 1965 |
Kosmos 96 (Russian : Космос 96 meaning Cosmos 96), or 3MV-4 No.6, was a Soviet spacecraft intended to explore Venus. A 3MV-4 spacecraft launched as part of the Venera programme, Kosmos 96 was to have made a flyby of Venus. However, due to a launch failure, it did not depart low Earth orbit. Its re-entry into Earth's atmosphere is often speculated as the cause of the Kecksburg UFO incident.
This was the third and last spacecraft prepared for a Venus encounter. The 3MV-4 No.6 spacecraft was originally built for a mission to Mars, with launch scheduled for late 1964. After it was not launched by the end of its launch window, the spacecraft was repurposed, along with two other spacecraft which were launched as Venera 2 and Venera 3, to explore Venus. [5]
The eight scientific instruments were:
A Molniya 8K78 s/n U15000-30 carrier rocket was used to launch 3MV-4 No.6. The launch occurred from Site 31/6 at the Baikonur Cosmodrome at 03:22 GMT on 23 November 1965. [6] Late in third stage flight, a fuel line ruptured, causing one of the engine's combustion chambers to explode. The rocket tumbled out of control, and as a result the fourth stage, a Blok-L, failed to ignite. The spacecraft was deployed into a low Earth orbit with a perigee of 227 kilometres (141 mi), an apogee of 310 kilometres (190 mi), an 51.9° of inclination, and an orbital period of 89.8 minutes. The spacecraft was named Kosmos 96, part of a series typically used for military and experimental satellites in order to cover up the failure. Had it departed Earth's orbit, it would have received the next designation in the Venera series, at the time Venera 4. Kosmos 96 was destroyed when it re-entered the Earth's atmosphere on 9 December 1965. [7]
There is some speculation that the re-entry of the Kosmos 96 (Venera-type spacecraft) was responsible for a fireball that was seen over southwestern Ontario, Canada, and at least eight US states from Michigan to New York at 21:43 GMT on 9 December 1965. Investigations of photographs and sightings of the fireball indicated its path through the atmosphere was probably too steep to be consistent with a spacecraft re-entering from Earth orbit and was more likely a meteor in a prograde orbit from the vicinity of the asteroid belt, and probably ended its flight over western Lake Erie. U.S. Air Force tracking data on Kosmos 96 also indicate the spacecraft orbit decayed earlier than 21:43 GMT on 9 December 1965. Other unconfirmed reports state the fireball subsequently landed in Pennsylvania southeast of Pittsburgh near the town of Kecksburg (40.2 N, 79.5 W) at 21:46 EST (although estimating the impact point of fireballs from eyewitness accounts is notoriously inaccurate). Uncertainties in the orbital information and re-entry coordinates and time make it difficult to determine definitively if the fireball could have been the Kosmos 96 spacecraft. [8]
Kosmos 21 was a Soviet spacecraft. This mission has been tentatively identified by NASA as a technology test of the Venera series space probes. It may have been an attempted Venus impact, presumably similar to the later Kosmos 27 mission, or it may have been intended from the beginning to remain in geocentric orbit. In any case, the spacecraft never left Earth orbit after insertion by the Molniya launcher. The orbit decayed on 14 November 1963, three days after launch.
Kosmos 27, also known as Zond 3MV-1 No.3 was a space mission intended as a Venus impact probe. The spacecraft was launched by a Molniya 8K78 carrier rocket from Baikonur. The Blok L stage and probe reached Earth orbit successfully, but the attitude control system failed to operate.
Venera 2, also known as 3MV-4 No.4 was a Soviet spacecraft intended to explore Venus. A 3MV-4 spacecraft launched as part of the Venera programme, it failed to return data after flying past Venus.
The 3MV planetary probe is a designation for a common design used by early Soviet unmanned probes to Mars and Venus. It was an incremental improvement of earlier 2MV probes and was used for Zond 1, Zond 2 and Zond 3 missions to Mars as well as several Venera probes. It was standard practice of the Soviet space program to use standardized components as much as possible. All probes shared the same typical characteristics and differed usually in equipment necessary for specific missions. Each probe also incorporated improvements based on experience with earlier missions.
Kosmos 101, also known as DS-P1-Yu No.4 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was built by the Yuzhnoye Design Bureau, and launched in 1965 as part of the Dnepropetrovsk Sputnik programme.
Kosmos 173, also known as DS-P1-Yu No.8 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was a 325 kilograms (717 lb) spacecraft, was built by the Yuzhnoye, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.
Kosmos 176, also known as DS-P1-Yu No.10 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was a 400 kilograms (880 lb) spacecraft, was built by the Yuzhnoye Design Office, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.
Kosmos 196, also known as DS-U1-G No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 352 kilograms (776 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used to study the effects of solar activity on the upper atmosphere.
Kosmos 95, also known as DS-U2-V No.2, was a Soviet satellite which was launched in 1965 as part of the Dnepropetrovsk Sputnik programme. The spacecraft weighed 325 kilograms (717 lb), and was built by the Yuzhnoye Design Office, and was used to conduct classified technology development experiments for the Soviet armed forces.
Kosmos 197, also known as DS-U2-V No.3, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 325 kilograms (717 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used to conduct classified technology development experiments for the Soviet armed forces.
Kosmos 145, also known as DS-U2-M No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 250 kilograms (550 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to conduct tests involving atomic clocks.
Kosmos 119, also known as DS-U2-I No.1, was a Soviet satellite which was launched in 1966 as part of the Dnepropetrovsk Sputnik programme. It was a 250 kilograms (550 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to study the effects on radio waves of passing through the ionosphere.
Kosmos 142, also known as DS-U2-I No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 315 kilograms (694 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to study the effects on radio waves of passing through the ionosphere.
Kosmos 163, also known as DS-U2-MP No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 357 kilograms (787 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used to investigate micrometeoroids and cosmic dust particles in near-Earth space.
Kosmos 167, or 4V-1 No.311, was a 1967 Soviet spacecraft intended to explore Venus. A spacecraft launched as part of the Venera programme, Kosmos 167 was intended to land on Venus but never departed low Earth orbit due to a launch failure.
Kosmos 20 or Zenit-2 No.13 was a Soviet optical film-return reconnaissance satellite which was launched in 1963. A Zenit-2 satellite, Kosmos 20 was the thirteenth of eighty-one such spacecraft to be launched.
Kosmos 32 or Zenit-2 No.18 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite which was launched in 1964. A Zenit-2 spacecraft, Kosmos 32 was the eighteenth of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb).
Kosmos 98 or Zenit-2 No.31 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1965. A Zenit-2 spacecraft, Kosmos 98 was the thirty-first of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb).
Kosmos 124 or Zenit-2 No.42 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 124 was the fortieth of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb).
Kosmos 147 or Zenit-2 No.44 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1967. A Zenit-2 spacecraft, Kosmos 147 was the forty-seventh of eighty-one such satellites to be launched. and had a mass of 4,000 kilograms (8,800 lb).