Luna (rocket)

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  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'.
  2. This is a transliteration of the sixth letter of the Cyrillic alphabet (E). A sense-for-sense translation would correspond to the sixth letter of the Latin alphabet, 'Block F'.

References

  1. "Soyuz - Version: Luna 8K72". Encyclopedia Astronautica. Archived from the original on 7 January 2010.
  2. "Vostok-L (8K72)". Gunter's Space Page. Retrieved 22 October 2023.
  3. "Tentatively Identified Missions and Launch Failures". NASA NSSDC. 6 January 2005.
  4. "Soyuz - Soyuz Chronology". Encyclopedia Astronautica. Archived from the original on 7 January 2010.
  5. "Luna 1 - NSSDC ID: 1959-012A". NASA.
  6. Reichl, Eugen (2017). Moskaus Mondprogramm. Paul Pietsch Verlage GmbH & Co (1. Auflage ed.). Stuttgart. ISBN   978-3-613-04027-4. OCLC   987572365.{{cite book}}: CS1 maint: location missing publisher (link)
Luna (8K727)
Block-E rocket stage.png
Block E upper stage, with Luna payload
Function Small-lift launch vehicle
Manufacturer OKB-1
Country of origin Soviet Union
Size
Mass277,000 kg (611,000 lb)
Stages3
Capacity
Payload to LEO
Mass4,000 kg (8,800 lb)
Associated rockets
Family R-7
Launch history
StatusRetired
Launch sites Baikonur, Site 1/5
Total launches9
Failure5
Partial failure1
First flight23 September 1958
Last flight16 April 1960
Carries passengers or cargo Luna probes
Boosters (First stage) – Block B, V, G & D [a]
No. boosters4
Powered by1× RD-107-8D74-1959
Maximum thrust990 kN (220,000 lbf)
Total thrust3,960 kN (890,000 lbf)
Burn time120 seconds
Propellant LOX / Kerosene