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Vela 2A



Vela 2A was one of two spin-stabilized (2 rev/sec) 144-kg satellites comprising the second launch in a series of six Vela launches. The orbits of the two satellites on each launch were basically circular at about 17 earth radii and were spaced 180 deg apart. Their objectives were to monitor nuclear weapons explosions in space and to study x-rays, gamma-rays, neutrons, magnetic fields, and charged particles over a wide range of energies from solar wind to cosmic ray as the satellites passed through interplanetary space, the bow shock, the magnetosheath, and the magnetotail. The satellite operated in either a real-time mode (one data frame/sec) or a memory store mode (one data frame every 256 sec). The spacecraft operated in the real-time mode about 40 percent of the time and in the store mode for the rest of the time unitl the next Vela launch. At this time, tracking priority was given to the new spacecraft, and the older spacecraft operated in the store mode only. There had been less and less data coverage of these satellites with each succeeding launch.

Alternate Names

  • Vela 2 (USAF)
  • 00836
  • Vela 3 (TRW)
  • Vela2A

Facts in Brief

Launch Date: 1964-07-17
Launch Vehicle: Atlas-Agena D
Launch Site: Cape Canaveral, United States
Mass: 150 kg

Funding Agency

  • Department of Defense-Department of the Air Force (United States)


  • Surveillance and Other Military
  • Space Physics
  • Astronomy

Additional Information

Questions and comments about this spacecraft can be directed to: Coordinated Request and User Support Office

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