Luna E-6 No.8

From Wikipedia, the free encyclopedia
Jump to: navigation, search

Molniya-L

Luna E-6 No.8
Mission type Lunar lander
Mission duration Failed to orbit
Spacecraft properties
Spacecraft type E-6
Manufacturer OKB-1
Launch mass 1,422 kilograms (3,135 lb)
Start of mission
Launch date 10 April 1965, (1965-04-10)
Rocket Molniya-L 8K78L s/n R103-26
Launch site Baikonur 1/5

Luna E-6 No.8, sometimes identified by NASA as Luna 1965A,[1] was a Soviet spacecraft which was lost in a launch failure in 1965. It was a 1,422-kilogram (3,135 lb) Luna E-6 spacecraft,[2] the seventh of twelve to be launched,[3] It was intended to be the first spacecraft to perform a soft landing on the Moon, a goal which would eventually be accomplished by the final E-6 spacecraft, Luna 9.

Luna E-6 No.8 was launched on 10 April 1965, atop a Molniya-L 8K78L carrier rocket, flying from Site 1/5 at the Baikonur Cosmodrome.[4] During third stage flight, a nitrogen pipeline in the oxidiser tank depressurised, which caused a loss of oxidiser flow to the engine and resulted in the engine cutting off. The spacecraft failed to achieve orbit, and the spacecraft disintegrated on reentry.[5] Prior to the release of information about its mission, NASA correctly identified that it had been an attempt to land a spacecraft on the Moon.[1]

References[edit]

  1. ^ a b Williams, David R. (6 January 2005). "Tentatively Identified Missions and Launch Failures". NASA NSSDC. Retrieved 30 July 2010. 
  2. ^ Wade, Mark. "Luna E-6". Encyclopedia Astronautica. Retrieved 27 July 2010. 
  3. ^ Krebs, Gunter. "Luna E-6". Gunter's Space Page. Retrieved 27 July 2010. 
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 27 July 2010. 
  5. ^ Wade, Mark. "Soyuz". Encyclopedia Astronautica. Retrieved 27 July 2010. 

External links[edit]