Vega 2

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8°30′S164°30′E / 8.5°S 164.5°E / -8.5; 164.5 (Vega 2)

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References

  1. 1 2 3 Asif Siddiqi (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF) (second ed.). NASA History Program Office. ISBN   978-1-626-83043-1.
  2. 1 2 "Vega 2". nssdc.gsfc.nasa.gov. NASA . Retrieved 22 July 2024.
  3. 1 2 "In Depth: Vega 2". solarsystem.nasa.gov. NASA . Retrieved 14 April 2015.
  4. 1 2 3 4 Paolo Ulivi; David M. Harland (2009). Robotic Exploration of the Solar System Part II: Hiatus and Renewal. Springer. pp. 90–92. ISBN   978-0-387-78904-0.
Vega 2
Vega model - Udvar-Hazy Center.JPG
A replica of the Vega spacecraft displayed at the Udvar-Hazy Center, Virginia, US
NamesVenera–Halley 2
Mission type Venus/Halley exploration
OperatorSoviet space program
COSPAR ID 1984-128A
1984-128E
1984-128F
SATCAT no. 15449
15856
15857
Mission durationLander: 56 minutes
Balloon: 2 days
Flyby: 2 years, 3 months and 3 days
Spacecraft properties
Spacecraft5VK No. 902
Spacecraft type 5VK
Manufacturer NPO Lavochkin
Launch mass4,840 kg (10,670 lb) [1]
Landing mass1,520 kg (3,350 lb)
Dimensions2.7 m × 2.3 m × 5.7 m (8.9 ft × 7.5 ft × 18.7 ft) (lander)
Start of mission
Launch dateDecember 21, 1984 (1984-12-21), 09:13:52 UTC [1]
Rocket Proton-K/D
Launch site Baikonur 200/40
Contractor Khrunichev
End of mission
Last contactMarch 24, 1987 [1]
Orbital parameters
Reference system Heliocentric
Eccentricity 0.17
Perihelion altitude 0.70 AU
Aphelion altitude 0.98 AU
Inclination 51.5°
Period 281 days
Flyby of Venus
Closest approachJune 15, 1985
Distance24,500 km (15,200 mi)