Zond 3 was a 1965 space probe which performed a flyby of the Moon's far side,[3] taking a number of quality photographs for its time. It was a member of the Soviet Zond program while also being part of the Mars 3MV project. It was unrelated to Zond spacecraft designed for manned circumlunar missions (Soyuz 7K-L1). It is believed that Zond 3 was initially designed as a companion spacecraft to Zond 2 to be launched to Mars during the 1964 launch window. The opportunity to launch was missed, and the spacecraft was launched on a Mars-crossing trajectory as a spacecraft test, even though Mars was no longer attainable.
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Mission type | Lunar science | ||||||||||||||
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Operator | OKB-1 | ||||||||||||||
COSPAR ID | 1965-056A ![]() | ||||||||||||||
SATCAT no. | 01454 | ||||||||||||||
Mission duration | 228 days | ||||||||||||||
Spacecraft properties | |||||||||||||||
Spacecraft type | 3MV-4 | ||||||||||||||
Manufacturer | OKB-1 | ||||||||||||||
Launch mass | 960 kg (2,120 lb) | ||||||||||||||
Start of mission | |||||||||||||||
Launch date | July 18, 1965, 14:38 (1965-07-18UTC14:38) UTC | ||||||||||||||
Rocket | Molniya SL-6/A-2-e | ||||||||||||||
Launch site | Baikonur LC-1/5 | ||||||||||||||
End of mission | |||||||||||||||
Last contact | March 3, 1966 (1966-03-04)[1] | ||||||||||||||
Orbital parameters | |||||||||||||||
Reference system | Heliocentric | ||||||||||||||
Eccentricity | 0.2683 | ||||||||||||||
Perihelion altitude | 0.9 AU (130 million km) | ||||||||||||||
Aphelion altitude | 1.56 AU (233 million km) | ||||||||||||||
Inclination | 0.5° | ||||||||||||||
Period | 500 days | ||||||||||||||
Epoch | July 19, 1965, 20:00 UTC[2] | ||||||||||||||
Flyby of Moon | |||||||||||||||
Closest approach | July 20, 1965 | ||||||||||||||
Distance | 9,219 km (5,728 mi) | ||||||||||||||
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Zond program None → |
The spacecraft was of the 3MV-4 type, similar to Zond 2.[1] In addition to a 106.4 mm focal length f/8 imaging system for visible light photography and ultraviolet spectrometry at 285-355 μm, it carried ultraviolet (190-275 μm) and infrared (3-4 μm) spectrophotometers, radiation sensors (gas-discharge and scintillation counters), charged particle detector, magnetometer, and micrometeoroid detector.[1][4] It also had an experimental ion engine.
Zond 3 was launched from Baikonur Cosmodrome on July 18, 1965, at 14:38 UTC, and was deployed from a Tyazhely Sputnik (65-056B) Earth-orbiting platform towards the Moon and interplanetary space. This was a repeat of a mission that failed in late 1963 intended to test communication at distances equivalent to the distances experienced by Mars and Earth.[5]
Zond 3's lunar flyby occurred on July 20 with a closest approach of 9,219 km (5,728 mi),[1] approximately 35 hours after launch. 25 visible light photographs and 3 ultraviolet spectra of very good quality were taken of the lunar surface, beginning at 01:24 UTC and 11,570 km (7,190 mi) prior to closest approach and ending at 02:32 UTC and 9,960 km (6,190 mi) past closest approach, covering a period of 68 minutes.[1][6] The photos covered 19 million km2 (7.3 million sq mi) of the lunar surface.[7]
Zond 3 proceeded on a trajectory across Mars' orbit, but not at a time when planetary encounter would occur. These images were transmitted by radio frequency on July 29 at a distance of 2.25 million km (1.40 million mi). To test telemetry, the camera film was rewound and retransmitted in mid-August, mid-September, and finally on October 23 at a distance of 31.5 million km (19.6 million mi), thus proving the ability of the communications system.[1] The subsequent transmissions were also at progressively slower data rates but higher quality.[5] The mission was ended after radio contact ceased on March 3, 1966, when it was at a distance of 153.5 million km (95.4 million mi).[1][4] It operated for 228 days, roughly equivalent to the time needed to survive a journey to Mars and exceeding that needed for Venus.[1]
Preceded by Zond 2 |
Zond program | Succeeded by None |
Zond program | ||
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3MV based missions | ![]() | |
Soyuz 7K-L1/L1S |
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Other |
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Cancelled / concepts |
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See also |
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← 1964 · Orbital launches in 1965 · 1966 → | |
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Kosmos 52 | OPS 3928 | OPS 7040 | OV1-1 | TIROS-9 | OPS 4703 | Kosmos 53 | OSO-2 | LES-1 | DS-P1-Yu No.2 | Apollo AS-103 · Pegasus 1 | Ranger 8 | DS-A1 No.6 | Kosmos 54 · Kosmos 55 · Kosmos 56 | Kosmos 57 | OPS 4782 | Kosmos 58 | Surveyor SD-1 | Kosmos 59 | NRL PL142 · GGSE-2 · GGSE-3 · SECOR 3 · Solrad 7B · Surcal 4 · Dodecapole 1 · OSCAR 3 | OPS 7087 · SECOR 2 | Kosmos 60 | OPS 4920 | Kosmos 61 · Kosmos 62 · Kosmos 63 | OPS 7353 | Voskhod 2 | Ranger 9 | Gemini III | Kosmos 64 | OPS 4803 | OPS 4682 · SECOR 4 | Intelsat I F1 | Luna E-6 No.8 | Kosmos 65 | Molniya 1-01 | OPS 4983 · OPS 6717 | Explorer 27 | OPS 5023 | LES-2 · LCS-1 | Kosmos 66 | Luna 5 | OPS 8431 | OPS 8386 | Apollo AS-104 · Pegasus 2 | Kosmos 67 | OPS 5236 | OV1-3 | Explorer 28 | Gemini IV | Luna 6 | OPS 8425 | Kosmos 68 | Titan 3C-7 | OPS 8480 | Kosmos 69 | OPS 5501 · OPS 6749 | TIROS-10 | Kosmos 70 | OPS 5810 | Zenit-2 No.28 | Kosmos 71 · Kosmos 72 · Kosmos 73 · Kosmos 74 · Kosmos 75 | Proton 1 | OPS 8411 | Zond 3 | OPS 5543 | OPS 6577 · OPS 6564 · ERS-17 | Kosmos 76 | Apollo AS-105 · Pegasus 3 | Kosmos 77 | OPS 5698 · OPS 6761 | SEV · SECOR 5 | Surveyor SD-2 | OPS 8464 · Dodecapole 2 · Tempsat-1 · Long Rod · Calsphere 4A · Surcal 5 | Kosmos 78 | OPS 7208 | Gemini V (REP) | Kosmos 79 | OSO-C | OPS 3373 | Kosmos 80 · Kosmos 81 · Kosmos 82 · Kosmos 83 · Kosmos 84 | Kosmos 85 | OPS 8068 | Kosmos 86 · Kosmos 87 · Kosmos 88 · Kosmos 89 · Kosmos 90 | OPS 7221 | Kosmos 91 | OPS 7208 | Luna 7 | OV1-2 | OPS 5325 | OGO-2 | Molniya 1-02 | OV2-1 · LCS-2 | Kosmos 92 | Kosmos 93 | GATV 5002 | Kosmos 94 | OPS 2155 | Proton 2 | Kosmos 95 | Explorer 29 | OPS 8293 · OPS 6232 | Venera 2 | Venera 3 | Solrad 8 | Kosmos 96 | Kosmos 97 | Astérix | Kosmos 98 | Alouette 2 · Explorer 31 | Luna 8 | Gemini VII | FR-1 | OPS 7249 | Kosmos 99 | Gemini VIA | Pioneer 6 | Kosmos 100 | Kosmos 101 | OV2-3 · LES-3 · LES-4 · OSCAR 4 | OPS 1509 | OPS 4639 | Kosmos 102 | Kosmos 103 | DS-K-40 No.1 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |