Vela 1A
USAF | |
| COSPAR ID | 1963-039A |
|---|---|
| SATCAT no. | 00674 |
| Mission duration | 6 months (planned) |
| Spacecraft properties | |
| Manufacturer | TRW |
| Launch mass | 150 kilograms (330 lb) |
| Power | 90 W |
| Start of mission | |
| Launch date | October 17, 1963, 02:24 |
| Rocket | LC-13 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Highly Elliptical |
| Perigee altitude | 101,081 kilometres (62,809 mi) |
| Apogee altitude | 116,582 kilometres (72,441 mi) |
| Inclination | 38.7° |
| Period | 6,486.2 minutes |
| Epoch | October 17, 1963 |
Vela 1A (or Vela 1) was a
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
magnetotail.[2]
See also
References
- ^ Wade, Mark. "Vela". Astronautix. Archived from the original on December 28, 2016. Retrieved June 1, 2018.
- ^ NASA Goddard Space Flight Center. "Vela 1A". Retrieved June 1, 2018.
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