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Sputnik 1

NSSDCA/COSPAR ID: 1957-001B

Description

The Sputnik 1 spacecraft was the first artificial satellite successfully placed in orbit around the Earth and was launched from Baikonur Cosmodrome at Tyuratam (370 km southwest of the small town of Baikonur) in Kazakhstan, then part of the former Soviet Union. The Russian word "Sputnik" means "companion" ("satellite" in the astronomical sense).

In 1885 Konstantin Tsiolkovsky first described in his book, Dreams of Earth and Sky, how such a satellite could be launched into a low altitude orbit. It was the first in a series of four satellites as part of the Sputnik program of the former Soviet Union and was planned as a contribution to the International Geophysical Year (1957-1958). Three of these satellites (Sputnik 1, 2, and 3) reached Earth orbit.

The Sputnik 1 satellite was a 58.0 cm-diameter aluminum sphere that carried four whip-like antennas that were 2.4-2.9 m long. The antennas looked like long "whiskers" pointing to one side. The spacecraft obtained data pertaining to the density of the upper layers of the atmosphere and the propagation of radio signals in the ionosphere. The instruments and electric power sources were housed in a sealed capsule and included transmitters operated at 20.005 and 40.002 MHz (about 15 and 7.5 m in wavelength), the emissions taking place in alternating groups of 0.3 s in duration. The downlink telemetry included data on temperatures inside and on the surface of the sphere.

Since the sphere was filled with nitrogen under pressure, Sputnik 1 provided the first opportunity for meteoroid detection (no such events were reported), since losses in internal pressure due to meteoroid penetration of the outer surface would have been evident in the temperature data. The satellite transmitters operated for three weeks, until the on-board chemical batteries failed, and were monitored with intense interest around the world. The orbit of the then inactive satellite was later observed optically to decay 92 days after launch (January 4, 1958) after having completed about 1400 orbits of the Earth over a cumulative distance traveled of 70 million kilometers. The orbital apogee declined from 947 km after launch to 600 km by Dec. 9th.

The Sputnik 1 rocket booster also reached Earth orbit and was visible from the ground at night as a first magnitude object, while the small but highly polished sphere, barely visible at sixth magnitude, was more difficult to follow optically. Several replicas of the Sputnik 1 satellite can be seen at museums in Russia and another is on display in the Smithsonian National Air and Space Museum in Washington, D.C.

Alternate Names

  • 00002

Facts in Brief

Launch Date: 1957-10-04
Launch Vehicle: Modified SS-6 (Sapwood)
Launch Site: Tyuratam (Baikonur Cosmodrome), U.S.S.R
Mass: 83.6 kg

Funding Agency

  • Unknown (U.S.S.R)

Disciplines

  • Earth Science
  • Space Physics

Additional Information

Questions or comments about this spacecraft can be directed to: Dr. David R. Williams.

 

Selected References

Eckels, A., et al., Ephemeris of satellite 1957 Alpha 2, In - IGY Satellite Rpt. Series, No. 8, June 15, 1959.

Warwick, J. W., Decay of spin in Sputnik 1, Planet. Space Sci., 1, 43-49, 1959.

Gindin, Ye. Z., et al., Optical observations of artificial earth satellites, In -- Prelim. Results of Sci. Res., 1-39, Nauka, Articles No. 1, Moscow, USSR, 1958.

King-Hele, D. G., Analysis of the orbits of the Russian satellites, Proc. Roy. Soc. London, A, 253, 529-538, 1959.

Govorchin, G. G., Soviets in space - an historical survey, Spaceflight, 7, 74-82, May 1965.

Harvey, B., The new Russian space programme from competition to collaboration, John Wiley & Sons, Chichester, England, 1996.

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