Sputnik 3
Credit: © Mark Wade
Russian earth magnetosphere satellite. 2 launches, 1958.04.27 (Sputnik failure) to 1958.05.15 (Sputnik 3). In July 1956 OKB-1 completed the draft project for the first earth satellite, designated ISZ (Artificial Earth Satellite).
The government go-ahead came in a decree of 3 September 1956. The Fourth Scientific Research Institute of the Ministry of Defense had meanwhile completed a draft project for the KIK ground control system. Tikhonravov's 1.4 metric ton ISZ satellite was to have been launched by the new R-7 ICBM as the Soviet Union's first satellite, but the R-7 was ready before the satellite, so it was preceded by Sputnik 1 and Sputnik 2. The ISZ was a miniature physics laboratory, but was launched with a known faulty recorder, limiting data to that received when the spacecraft was over Soviet tracking stations. As a result, the Van Allen radiation belts were discovered by the United States rather than Russia.
AKA: ISZ.
Gross mass: 1,327 kg (2,925 lb).
First Launch: 1958.04.27.
Last Launch: 1958.05.15.
Number: 2 .
More... - Chronology...
Associated Countries
See also
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Soyuz The Russian Soyuz spacecraft has been the longest-lived, most adaptable, and most successful manned spacecraft design. In production for fifty years, more than 240 have been built and flown on a wide range of missions. The design will remain in use with the international space station well into the 21st century, providing the only manned access to the station after the retirement of the shuttle in 2011. More...
Associated Launch Vehicles
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R-7 Russian intercontinental ballistic missile. The world's first ICBM and first orbital launch vehicle. The 8K71 version was never actually put into military service, being succeeded by the R-7A 8K74. More...
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Soyuz Russian orbital launch vehicle. The world's first ICBM became the most often used and most reliable launch vehicle in history. The original core+four strap-on booster missile had a small third stage added to produce the Vostok launch vehicle, with a payload of 5 metric tons. Addition of a larger third stage produced the Voskhod/Soyuz vehicle, with a payload over 6 metric tons. Using this with a fourth stage, the resulting Molniya booster placed communications satellites and early lunar and planetary probes in higher energy trajectories. By the year 2000 over 1,628 had been launched with an unmatched success rate of 97.5% for production models. Improved models providing commercial launch services for international customers entered service in the new millenium, and a new launch pad at Kourou was to be inaugurated in 2009. It appeared that the R-7 could easily still be in service 70 years after its first launch. More...
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Sputnik 8A91 Russian intercontinental ballistic orbital launch vehicle. Modified R-7 ICBM used to launch Sputnik 3. More...
Associated Manufacturers and Agencies
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Korolev Russian manufacturer of rockets, spacecraft, and rocket engines. Korolev Design Bureau, Kaliningrad, Russia. More...
Bibliography
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McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
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JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
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Varfolomyev, Timothy, "Soviet Rocketry that Conquered Space - Part 1", Spaceflight, 1995, Volume 37, page 260.
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Chertok, Boris Yevseyevich, Raketi i lyudi, Mashinostroenie, Moscow, 1994-1999.. Web Address when accessed: here.
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Melnik, T G, Voenno-Kosmicheskiy Siliy, Nauka, Moscow, 1997..
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Siddiqi, Asif A, The Soviet Space Race With Apollo, University Press of Florida, 2003.
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Grimwood, James M., Project Mercury: A Chronology, NASA Special Publication-4001.
Associated Launch Sites
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Baikonur Russia's largest cosmodrome, the only one used for manned launches and with facilities for the larger Proton, N1, and Energia launch vehicles. The spaceport ended up on foreign soil after the break-up of Soviet Union. The official designations NIIP-5 and GIK-5 are used in official Soviet histories. It was also universally referred to as Tyuratam by both Soviet military staff and engineers, and the US intelligence agencies. Since the dissolution of the Soviet Union the Russian Federation has insisted on continued use of the old Soviet 'public' name of Baikonur. In its Kazakh (Kazak) version this is rendered Baykonur. More...
Sputnik 3 Chronology
1952 May 16 - .
- International Geophysical Year Committee established. - .
Nation: USA. Spacecraft: Vanguard 2; Sputnik 3. Summary: The Special Committee for the International Polar Year (later designated the International Geophysical Year), was established..
1956 January 30 - .
- Development of first Sputnik authorised. - .
Nation: USSR. Spacecraft: Sputnik 3. Summary: Central Committee of the Communist Party and Council of Soviet Ministers Decree 149882 'On creation of the Object D artificial satellite' was issued..
1956 July - .
LV Family:
R-7.
Launch Vehicle:
R-7.
- OKB-1 completed draft project for the first earth satellite - .
Nation: USSR. Spacecraft: Sputnik 3. Tikhonravov's unit of OKB-1 completed the preliminary design of the ISZ satellite (launched as Sputnik 3). The Fourth Scientific Research Institute of the Ministry of Defence had meanwhile completed a draft project for the KIK ground control system. Tikhonravov's 1.4 tonne ISZ satellite was to have been launched by the new R-7 ICBM as the Soviet Union's first satellite, but the R-7 was ready before the satellite, so it was preceded by Sputnik 1 and Sputnik 2. The ISZ was a miniature physics laboratory, but was launched with a known faulty recorder, limiting data to that received when the spacecraft was over Soviet tracking stations. As a result, the Van Allen radiation belts were discovered by the United States rather than Russia.
1956 September 3 - .
LV Family:
R-7.
Launch Vehicle:
R-7.
- Soviet space and ballistic missile tracking network established. - .
Nation: USSR. Spacecraft: Sputnik 3. Decree 1241-632 '0n creation or the Command Measurement Complex' was issued. The decree marked the beginning of development of the KIK satellite tracking system. This network was put together using a combination of PVO (Air Defence) and ICBM tracking systems. Trajectory information was fed into the KIK Centre for orbital calculations. The Centre was staffed by 680 officers and 151 civilian scientists of the Soviet Army in four sections.
1956 September 30 - .
LV Family:
R-7.
Launch Vehicle:
R-7.
- Sputnik 3 draft project approved. - .
Nation: USSR. Spacecraft: Sputnik 3. Decree 'On approval of the draft project for Object D' was issued. The decree gave the go-ahead for Tikhonravov's 1.4 tonne ISZ physics satellite to be launched by the new R-7 ICBM during the International Geophysical Year . The ISZ, a miniature physics laboratory,.was to have been the first artificial satellite of the earth. In the event, it was preceded by Sputniks 1 and 2.
1956 September 30 - .
LV Family:
N1;
Proton.
- First official plan for future Soviet spaceflight - .
Nation: USSR. Spacecraft: Sputnik 3; Vostok; Zenit-2. This set forth the following objectives: orbiting of satellites of 1.8 to 2.5 tonnes mass by 1958; one week flight of a manned spacecraft by 1964; unmanned reconnaissance satellite by 1970; rocket capable of 12 tonne escape velocity payload by 1970; rocket with 100 tonne low earth orbit payload to be developed, capable of placing 2 to 3 men on the moon (no date set).
1958 April 27 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Sputnik 8A91.
LV Configuration: Sputnik 8A91 B1-2.
FAILURE: Launch vehicle disintegrated 88 seconds after liftoff..
Failed Stage: 0.
- Sputnik failure - .
Payload: D-1 s/n 1. Nation: USSR. Agency: MVS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Sputnik 3. Decay Date: 1958-04-01 . COSPAR: F580427A.
1958 May 15 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Sputnik 8A91.
LV Configuration: Sputnik 8A91 B1-1.
- Sputnik 3 - .
Payload: D-1 s/n 2. Mass: 1,327 kg (2,925 lb). Nation: USSR. Agency: MVS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Sputnik 3. Decay Date: 1960-04-06 . USAF Sat Cat: 8 . COSPAR: 1958-Delta-2. Apogee: 1,864 km (1,158 mi). Perigee: 217 km (134 mi). Inclination: 65.2000 deg. Period: 106.00 min. Summary: Variety of scientific data. Research in the upper atmosphere and outer space.
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