The Vega program (Russian: Вега) was a series of Venus missions that also took advantage of the appearance of Halley's Comet in 1986. Vega 1 and Vega 2 were uncrewed spacecraft launched in a cooperative effort among the Soviet Union, who also provided the spacecraft and launch vehicle, Austria, Bulgaria, France, Hungary, the German Democratic Republic, Poland, Czechoslovakia, and the Federal Republic of Germany in December 1984. They had a two-part mission to investigate Venus, where each would release a lander and a balloon probe, and later conduct a flyby of Halley's Comet. The flyby of Halley's Comet had been a late mission change in the Venera program, following on from the cancellation of the American Halley mission in 1981. A later Venera mission was canceled and the Venus part of the Vega 1 mission was reduced. Because of this, the craft was designated VeGa, a contraction of Venera and Gallei (Венера and Галлей respectively, the Russian words for "Venus" and "Halley"). The spacecraft design was based on the previous Venera 9 and Venera 10 missions. The two spacecraft were launched on 15 and 21 December 1984, respectively. With their redesignated dual missions, the Vega probes became part of the Halley Armada, a group of space probes that studied Halley's Comet during its 1985/1986 perihelion. The balloon probes that both missions released into the Venusian atmosphere were also the first man-made aircraft to fly on a planet other than Earth, albeit unpowered, and until the operation of NASA's Ingenuity helicopter probe in 2021 the only examples of man-made extraterrestrial aircraft in history.
The Vega spacecraft
Vega 1 and Vega 2 were identical sister ships developed from the earlier Venera craft. They were of the 5VK type, designed by Babakin Space Center and constructed by Lavochkin at Khimki. The craft were powered by twin large solar panels and instruments included an antenna dish, cameras, spectrometer, infrared sounder, magnetometers (MISCHA; Austrian and Soviet), and plasma probes. The 4,920 kg (10,850 lb) craft were launched by a Proton 8K82K rocket from Baikonur Cosmodrome, Tyuratam, Kazakh SSR (current Kazakhstan). Both Vega 1 and Vega 2 were three-axis stabilized spacecraft. The spacecraft were equipped with a dual bumper shield for dust protection from Halley's comet.
Bus Instruments
The Venus mission Vega 1 arrived at Venus on 11 June 1985 and Vega 2 on 15 June 1985, and each delivered a 1,500 kg (3,300 lb), 240 cm (94 in) diameter spherical descent unit. The units were released some days before each arrived at Venus and entered the atmosphere without active inclination changes. Each contained a lander and a balloon explorer.
Descent craft
The landers were identical to that of the previous five Venera missions and were to study the atmosphere and surface. Each had instruments to study temperature and pressure, a UV spectrometer, a water concentration meter, a gas-phase chromatograph, an X-ray spectrometer, a mass spectrometer, and a surface sampling device. The Vega 1 lander's surface experiments were inadvertently activated at 20 km (12 mi) from the surface by an especially hard wind jolt, and so failed to provide results. It landed at 7.5°N, 177.7°E. The Vega 2 lander touched down at 03:00:50 UT on 15 June 1985 at 8.5° S, 164.5° E, in eastern Aphrodite Terra. The altitude of the touchdown site was 0.1 km (0.062 mi) above the planetary mean radius. The measured pressure at the landing site was 91 atm and the temperature was 736 K (463 °C; 865 °F). The surface sample was found to be an anorthosite-troctolite. The lander transmitted data from the surface for 56 minutes.
Payload
Balloon
The two balloon aerobots were designed to float at 54 km (34 mi) from the surface, in the most active layer of the Venusian cloud system. The instrument pack had enough battery power for 60 hours of operation and measured temperature, pressure, wind speed, and aerosol density. The balloon envelopes were surfaced with polytetrafluoroethylene to resist attack by the corrosive atmosphere. Both Vega-1 and Vega-2 balloons operated for more than 46 hours from injection to the final transmission. The balloons were of spherical superpressure types of 3.54 m (11.6 ft) diameter, filled with helium. A gondola assembly weighing 6.9 kg (15 lb) and 1.3 m (4 ft 3 in) long was connected to the balloon envelope by a tether 13 m (43 ft) long. Total mass of the entire assembly was 21 kg (46 lb). The top section of the gondola assembly was capped by a conical antenna 37 cm (15 in) tall and 13 cm (5.1 in) wide at the base. Beneath the antenna was a module containing the radio transmitter and system control electronics. The lower section of the gondola assembly carried the instrument payload and batteries. The instruments consisted of:
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