Vega 1

Vega 1
Vega Solar System probe bus and landing apparatus (model)
NamesVenera-Halley 1
Mission typePlanetary science including lander and atmospheric probe
OperatorSoviet Academy of Sciences
COSPAR ID
SATCAT no.
  • 15432
  • 15858
  • 15859
Mission durationBalloon: 2 days
Orbiter: 2 years, 1 month and 15 days
Spacecraft properties
Spacecraft5VK No. 901
Spacecraft type5VK
ManufacturerNPO Lavochkin
Launch mass4,840 kilograms (10,670 lb)[1]
Start of mission
Launch dateDecember 15, 1984 (1984-12-15), 09:16:24 UTC[1]
RocketProton 8K82K
Launch siteBaikonur 200/39
End of mission
Last contact30 January 1987[2]
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis6,558 kilometres (4,075 mi)
Eccentricity0.03080
Perigee altitude159 kilometres (99 mi)
Apogee altitude202 kilometres (126 mi)
Inclination51.5°
Period88 minutes
Flyby of Venus
Closest approach11 June 1985
Distance~39,000 kilometres (24,000 mi)
Venus atmospheric probe
Spacecraft componentVega 1 Balloon
Atmospheric entry02:06:10, 11 June 1985
Venus lander
Spacecraft componentVega 1 Descent Craft
Landing date03:02:54, 11 June 1985
Landing site7°30′N 177°42′E / 7.5°N 177.7°E / 7.5; 177.7 (Vega 1) (north of Aphrodite Terra)
Flyby of 1P/Halley
Closest approach6 March 1986
Distance~10,000 km (6,200 mi)

Insignia of the mission
← None
Vega 2 →
 

Vega 1 (along with its twin Vega 2) was a Soviet space probe, part of the Vega program. The spacecraft was a development of the earlier Venera craft. They were designed by Babakin Space Centre and constructed as 5VK by Lavochkin at Khimki. The name VeGa (ВеГа) combines the first two letters from the Russian words for Venus (Венера: "Venera") and Halley (Галлея: "Galleya").

The craft was powered by twin large solar panels and instruments included an antenna dish, cameras, spectrometer, infrared sounder, magnetometers (MISCHA), and plasma probes. The 4,840 kilograms (10,670 lb) craft was launched by a Proton 8K82K rocket from Baikonur Cosmodrome, Tyuratam, Kazakh SSR. Both Vega 1 and 2 were three-axis stabilized spacecraft. The spacecraft were equipped with a dual bumper shield[3] for dust protection from Halley's comet.

  1. ^ a b "Vega 1" (PDF). NASA. Retrieved 2022-12-02.
  2. ^ NASA.gov
  3. ^ V. A. Agureikin, S. I. Anisimov, A. V. Bushman, G. I. Kanel', V. P. Karyagin, A. B. Konstantinov, B. P. Kryukov, V. F. Minin, S. V. Razorenov, R. Z. Sagdeev, S. G. Sugak, V. E. Fortov, (1984). "Thermo-physical and gas-dynamic studies of the meteorite shield for the Vega spacecraft". High Temperature 761-778 22(5). WoS:A1984ALC5000020 Scopus:2-s2.0-0021489019

© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search