- Mars 1
This is for a Soviet space probe, for moon designated as Mars I, see Phobos (moon).This is for a Soviet space probe, for a Chinese space probe sometimes referred to as Mars 1, see Yinghuo-1.
Mars 1, also known as 1962 Beta Nu 1, Mars 2MV-4 and Sputnik 23, was an automatic interplanetary station launched in the direction of Mars on November 1, 1962, the first of the Soviet Mars probe program, with the intent of flying by the planet at a distance of about 11,000 km. It was designed to image the surface and send back data on cosmic radiation, micrometeoroid impacts and Mars' magnetic field, radiation environment, atmospheric structure, and possible organic compounds. After leaving Earth orbit, the spacecraft and the booster fourth stage separated and the solar panels were deployed. Early telemetry indicated that there was a leak in one of the gas valves in the orientation system so the spacecraft was transferred to gyroscopic stabilization. Sixty-one radio transmissions were held, initially at two day intervals and later at five days in which a large amount of interplanetary data were collected. On 21 March 1963, when the spacecraft was at a distance of 106,760,000 km from Earth on its way to Mars, communications ceased, probably due to failure of the spacecraft's antenna orientation system. Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit.
Mars 1 was a modified Venera-type spacecraft in the shape of a cylinder 3.3 m long and 1.0 m in diameter. The spacecraft measured 4 metretres across with the solar panels and radiators deployed. The cylinder was divided into two compartments. The upper 2.7 m, the orbital module, contained guidance and on-board propulsion systems. The experiment module, containing the scientific instrumentation, comprised the bottom 0.6 m of the cylinder. A 1.7 m parabolic high gain antenna was used for communication, along with an omnidirectional antenna and a semi-directional antenna. Power was supplied by two solar panel wings with a total area of 2.6 square meters affixed to opposite sides of the spacecraft. Power was stored in a 42 ampere-hour cadmium-nickel battery.
Communications were via a decimeter wavelength radio transmitter mounted in the orbital module which used the high-gain antenna. This was supplemented by a metre wavelength range transmitter through the omnidirectional antenna. An 8 centimetre wavelength transmitter mounted in the experiment module was designed to transmit the TV images. Also mounted in the experiment module was a 5-centimeter range impulse transmitter. Temperature control was achieved using a binary gas-liquid system and hemispherical radiators mounted on the ends of the solar panels. The craft carried various scientific instruments including a magnetometer probe, television photographic equipment, a spectroreflexometer, radiation sensors (gas-discharge and scintillation counters), a spectrograph to study ozone absorption bands, and a micrometeoroid instrument.
The probe recorded one micrometeorite strike every two minutes at altitudes ranging from 6000 to 40,000 km due to the Taurids meteor shower and also recorded similar densities at distances from 20 to 40 million km. Magnetic field intensities of 3–4 nanoteslas (nT, also known as gammas) with peaks as high as 6–9 nT were measured in interplanetary space and the solar wind was detected. Measurements of cosmic rays showed that their intensity had almost doubled since 1959. The radiation zones around the Earth were detected and their magnitude confirmed.
This spacecraft is also referenced as Sputnik 23 and Mars 2MV-4. It was originally designated Sputnik 30 in the U.S. Naval Space Command Satellite Situation Summary.
- Exploration of Mars
- Space exploration
- Unmanned space missions
- Marsnik program
- The Soviet Mars program, Professor Chris Mihos, Case Western Reserve University
Failed and cancelled Mars missions Failed at launch Failed en routeMars 1 · Zond 2 · Mars 6 · Mars 7 · Phobos 1 · Mars Observer · Nozomi · Mars Climate Orbiter · Mars Polar Lander · Deep Space 2 · Beagle 2 Cancelled (year cancelled)Voyager · Marsokhod (Mars 4NM) · Mars sample return (Mars 5NM) · Mars Surveyor 2001 Lander · NetLander · Mars Telecommunications Orbiter · Beagle 3 · Mars Astrobiology Explorer-Cacher (2011) ← 1961 · Orbital launches in 1962 · 1963 →Discoverer 37 | Solrad 4 · LOFTI 2A · SECOR · Injun 2 · Surcal 1 | Ranger 3 | TIROS-4 | Mercury-Atlas 6 | FTV-2301 | Discoverer 38 | OSO-1 | Samos 6 | Kosmos 1 | Kosmos 2 | Midas 5 · Westford Drag | FTV-1142 | Ranger 4 | Kosmos 3 | Solrad 4B | Kosmos 4 | Ariel 1 | FTV-2401 | FTV-1125 | ANNA 1A | FTV-1126 | FTV-3501 | Mercury-Atlas 7 (Balloon Subsatellite 1) | FTV-3501 | Kosmos 5 | FTV-1128 | Zenit-2 No.3 | FTV-1127 · Oscar 2 | FTV-2402 | FTV-2312 | TIROS-5 | FTV-1129 | FTV-1151 | Kosmos 6 | Telstar 1 | FTV-2403 | FTV-1130 | Mariner 1 | FTV-1131 | Kosmos 7 | FTV-1152 | FTV-2404 | Vostok 3 | Vostok 4 | Kosmos 8 | FTV-2502 | Venera 2MV-1 No.1 | Mariner 2 | FTV-1153 | Venera 2MV-1 No.2 | FTV-1132 | Venera 2MV-2 No.1 | FTV-1133 · ERS-2 | TIROS-6 | Kosmos 9 | Alouette 1 · TAVE | FTV-1154 | Explorer 14 | Mercury-Atlas 8 | FTV-1134 | Kosmos 10 | Ranger 5 | Kosmos 11 | Mars 2MV-4 No.1 | 1MS No.2 | STARAD | Explorer 15 | ANNA 1B | Mars 1 | Mars 2MV-3 No.1 | FTV-1136 | FTV-2405 · ERS-1 | FTV-1135 | FTV-1155 | NRL PL120 · Injun 3 · NRL PL121 · Surcal 2 · Calsphere 1 | Relay 1 | FTV-1136 | Explorer 16 | Midas 6 · ERS-3 · ERS-4 | Transit 5A-1 | Kosmos 12Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets.Categories:
- Mars spacecraft
- Soviet Mars probe program
- Artificial satellites orbiting Sun
- Inactive extraterrestrial probes
- 1962 in spaceflight
- 1962 in the Soviet Union
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