Sputnik (rocket)

Last updated
  1. This is a transliteration of the second through fifth letters of the Cyrillic alphabet (Б, В, Г, Д). A sense-for-sense translation would correspond to the second through fifth letters of the Latin alphabet, 'Block B, C, D & E'.

References

  1. (in Russian) Sputnik Rocket Archived 2005-01-03 at the Wayback Machine
  2. "РД-107 и РД-108 | RD-107 and RD-108". lpre.de. Retrieved 2015-12-24.
  3. "Jonathan McDowell's launch log". planet4589.org. Retrieved 2015-12-24.
  4. (in Russian) Soviet Solar Cells on Orbit
  5. "Sputnik 3". astronautix.com. Archived from the original on 2013-11-08. Retrieved 2015-12-24.
  6. "Sputnik 8A91". astronautix.com. Retrieved 13 May 2023.
  7. "SL-1 R/B". n2yo.com.
Sputnik 8K71PS grey.svg
Sputnik rocket
FunctionEarly (first) carrier rocket
Manufacturer OKB-1
Country of originUSSR
Size
Height8K71PS: 30  m (98  ft)
8A91: 31.1 m (102 ft)
Diameter2.99 m (9 ft 10 in)
Width10.303 m (33.80 ft)
Mass8K71PS: 267,000 kg (589,000 lb)
8A91: 269,300 kg (593,700 lb)
Stages3
Capacity
Payload to LEO
Mass8K71PS: 500 kg (1,100 lb)
8A91: 1,327 kg (2,926 lb)
Associated rockets
Family R-7
Comparable Vanguard
Juno I
Launch history
StatusRetired
Launch sites Baikonur, Site 1/5
Total launches4 (8K71PS: 2, 8A91: 2)
Success(es)3
Failure1 (8A91)
First flight8K71PS: 4 October 1957
8A91: 27 April 1958
Last flight8K71PS: 3 November 1957
8A91: 15 May 1958
Carries passengers or cargo Sputnik 1
Sputnik 2
Sputnik 3
Boosters (First stage) – Block B, V, G & D [a]
No. boosters4
Powered by1× RD-107
Maximum thrust970  kN (220,000  lbf)
Specific impulse 306 s (3.00 km/s)
Burn time120 seconds
Propellant LOX / Kerosene