Sputnik 3

Source: Wikipedia, the free encyclopedia.
Sputnik 3
OKB-1
Harvard designation1958 Delta 2
COSPAR ID1958-004B Edit this at Wikidata
SATCAT no.00008
WebsiteNASA NSSDC Master Catalog
Mission duration692 days
Spacecraft properties
Manufacturer
Korolev Design Bureau
Launch mass1,327 kilograms (2,926 lb)
Start of mission
Launch date15 May 1958, 07:12:00 (1958-05-15UTC07:12Z) UTC
Rocket
1/5
End of mission
Decay dateApril 6, 1960
Orbital parameters
Reference system
Semi-major axis
7,418.7 kilometres (4,609.8 mi)
Eccentricity0.110932
Perigee altitude217 kilometres (135 mi)
Apogee altitude1,864 kilometres (1,158 mi)
Inclination65.18°
Period105.9 minutes
Epoch15 May 1958 07:12:00 UTC
Sputnik program
 
Instruments
Quadrupole Mass Spectrometer Composition of the upper atmosphere
Ionization and Magnetic Manometer Pressure of the upper atmosphere
Geiger counters Charged particles
Piezo-Electric Meteorite Counter Micrometeoroids
Fluxgate Magnetometer Magnetic field
Field Mill Electrometer Electric field
Universal newsreel about the Soviet Union's Industrial Exhibition in 1958 featuring a replica of Sputnik 3

Sputnik 3 (

near space
.

1958 Soviet Union stamp

Sputnik 3 was the only Soviet satellite launched in 1958. Like its American counterpart, Vanguard 1, Sputnik 3 reached orbit during the International Geophysical Year.[1]

History

On 30 January 1956, the

OKB-1 had completed the preliminary design,[4][5] but modifications to the R-7 for a satellite launch was ready before Object D could be finished. Worried at the prospect of the United States launching a satellite before he could, Sergei Korolev decided that the relatively simple "Prosteyshiy Sputnik-1" ("Simple Satellite 1", or PS-1), also known as Sputnik 1, would be the first satellite to be launched instead. Sputnik 2
(PS-2) was also ready and therefore launched earlier than Object D.

Launch

Sputnik 3 was launched by a modified R-7 Semyorka missile developed for satellite launches, the Sputnik 8A91.[8]

The 8A91 was a transitional design between the initial 8K71 test model R-7 and the operational 8K74, which had yet to fly. Improvements in manufacturing processes were used to reduce the gauge of the slosh baffles in the propellant tanks and cut down on weight. The engines were slightly more powerful and the changes in mass resulted in modifications to the flight plan--the core stage would be throttled down and the strap-ons throttled up 25% prior to their jettison. An interstage section replaced the radio equipment bay at the top of the booster, and the telemetry package was also moved here.

The launch was planned for 20 April, but technical delays meant that several more days were needed. On 27 April, the 8A91 booster lifted from LC-1 and all appeared normal for over a minute into the launch. Around 1+1⁄2 minutes, things went awry. The strap-on boosters broke away from the core and the entire launch vehicle tumbled to earth 224 km (139 mi) downrange. Ground crews monitoring radar tracking data from the booster noticed the trajectory angle change to negative numbers, followed by a complete loss of signal. The last data packet received indicated that the booster had flown only 227 kilometers at signal loss.

Telemetry data indicated that abnormal vibrations began affecting the booster at T+90 seconds and vehicle breakup occurred seven seconds later. A search plane located the impact site. It was not clear what had caused the vibrations, but the decision was made to go ahead with the backup booster and satellite. The engines would be throttled down at T+85 seconds in the hope of reducing structural loads. Since the booster did not carry sufficient instrumentation to determine the source of the vibrations, which ultimately proved to be a phenomenon resulting from the propellant tanks emptying, it would end up being a recurring problem on lunar probe launches later in the year.

The satellite had separated from the launch vehicle and was recovered near the crash site largely intact. It was taken back to the Baikonur Cosmodrome for refurbishment, but an electrical short started a fire inside the electronics compartment and it could not be reused.

The backup booster and satellite were launched successfully on the morning of 15 May, specifically chosen as it was the anniversary of the R-7's maiden flight. On the downside, telemetry data indicated that vibration affected the launch vehicle again and it came close to meeting the same fate as its predecessor.

Spacecraft

While no Soviet satellite had been in orbit since the end of Sputnik 2 in April 1958, Sputnik 3 weighed about 100 times as much as the heaviest of the three active American satellites, and exceeded their combined scientific-data abilities.[9] It was an automatic scientific laboratory spacecraft. It was conically shaped and was 3.57 m (11.7 ft) long and 1.73 m (5.68 ft) wide at its base. The satellite weighed 1,327 kg (1.46 tons) and carried twelve scientific instrumentation. After 692 days in orbit, Sputnik 3 reentered the atmosphere and burned up on 6 April 1960.[10] It was powered by silver-zinc batteries and silicon solar cells which operated for approximately 6 weeks.[11][12]

Mission

Sputnik 3 included twelve scientific instruments that provided data on pressure and composition of the upper

meteoric particles.[10] The onboard Tral-D tape recorder, intended to store data for later transmission to Earth failed, limiting data to what could be gathered while the satellite was directly visible from ground stations. Because of this failure, Sputnik 3 was unable to map the Van Allen radiation belt.[13][14]

See also

Footnotes

  1. ^ Green, Constance McLaughlin, and Lomax, Milton.. Vanguard a History, Washington D.C., National Aeronautics and Space Administration, 1970, p. 219. NASA SP-4202
  2. ^ a b c Siddiqi, Asif A. (2023-03-29). "Korolev, Sputnik, and The International Geophysical Year". NASA History Division: Sputnik and the Dawn of the Space Age. National Aeronautics and Space Administration.
  3. ISBN 1-58834-007-4
  4. ^
    ISBN 0-8130-2627-X
  5. ^ a b Siddiqi, Asif A (2000). Challenge To Apollo: The Soviet Union and The Space Race, 1945-1974 (PDF). NASA. p. 151.
  6. ISBN 0-8130-2627-X
  7. ISBN 0-471-14853-9
  8. ISBN 0-8130-2627-X
  9. ^ "Sputnik and a Jumbo Space Lab". Life. 1958-05-26. pp. 119–120. Retrieved 2023-05-13.
  10. ^ a b "Sputnik 3 - Scientific Laboratory". Robert Christy. Retrieved 2011-06-30.
  11. ^ "USSR launches Sputnik-3". Retrieved 2020-08-24.
  12. ^ Mitchell, Don. "Sputnik-3". Retrieved 2020-08-24.
  13. ISBN 0-8130-2627-X
  14. ISBN 0-471-14853-9

References

External links
Retrieved from "https://en.wikipedia.org/w/index.php?title=Sputnik_3&oldid=1164865167"