Vela 1A

Vela 1A
Vela 1A
OperatorUSAF
COSPAR ID1963-039A Edit this at Wikidata
SATCAT no.00674
Mission duration6 months (planned)
Spacecraft properties
ManufacturerTRW
Launch mass150 kilograms (330 lb)
Power90 W
Start of mission
Launch dateOctober 17, 1963, 02:24 (1963-10-17UTC02:24Z)
RocketAtlas-LV3 Agena-D
Launch siteCape Canaveral LC-13
Orbital parameters
Reference systemGeocentric
RegimeHighly Elliptical
Perigee altitude101,081 kilometres (62,809 mi)
Apogee altitude116,582 kilometres (72,441 mi)
Inclination38.7°
Period6,486.2 minutes
EpochOctober 17, 1963 (1963-10-17)
Vela
← None
Vela 1B →
 

Vela 1A (or Vela 1) was a military satellite developed to detect nuclear detonations to monitor compliance with the 1963 Partial Test Ban Treaty by the Soviet Union.

Launch

Vela 1A was launched on October 17, 1963 from the Cape Canaveral Air Force Station, Florida, by an Atlas-Agena launch vehicle. Vela 1A was launched along with Vela 1B and with ERS 12.[1]

Mission

Vela 1A was a spin-stabilized 124-kg satellite comprising the first launch in a series of six Vela launches. Together with its twin Vela 1B, their objectives were to monitor nuclear weapons explosions in space and to study x-rays, gamma-rays, neutrons, and charged particles as the satellites passed through interplanetary space, the bow shock, the magnetosheath, and the magnetotail.[2]

See also

  • Vela (satellite)

References

  1. ^ Wade, Mark. "Vela". Astronautix. Archived from the original on December 28, 2016. Retrieved June 1, 2018.
  2. ^ NASA Goddard Space Flight Center. "Vela 1A". Retrieved June 1, 2018.
  • v
  • t
  • e
Orbital launches in 1963
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).
Stub icon

This spacecraft or satellite related article is a stub. You can help Wikipedia by expanding it.

  • v
  • t
  • e