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Zond 1
Soviet spacecraft launched in 1964 to explore Venus
Soviet spacecraft launched in 1964 to explore Venus
| Field | Value | |||||||
|---|---|---|---|---|---|---|---|---|
| name | Zond 1 | |||||||
| names_list | Zond 3MV-1 No. 4 | |||||||
| image | Zond 2.jpg | |||||||
| image_caption | The Russian Zond 1 | |||||||
| image_alt | ||||||||
| image_size | ||||||||
| mission_type | Venus lander | |||||||
| operator | OKB-1 | |||||||
| Harvard_designation | ||||||||
| COSPAR_ID | 1964-016D | |||||||
| SATCAT | 00785 | |||||||
| website | ||||||||
| mission_duration | ||||||||
| distance_travelled | ||||||||
| orbits_completed | ||||||||
| suborbital_range | ||||||||
| suborbital_apogee | ||||||||
| spacecraft | ||||||||
| spacecraft_type | ||||||||
| spacecraft_bus | 3MV-1 | |||||||
| manufacturer | ||||||||
| launch_mass | 890 kg | |||||||
| BOL_mass | ||||||||
| landing_mass | ||||||||
| dry_mass | 290 kg | |||||||
| payload_mass | ||||||||
| dimensions | 3.6 m tall | |||||||
| 1.1 m diameter | ||||||||
| power | ||||||||
| launch_date | ||||||||
| launch_rocket | Molniya 8K78M | |||||||
| launch_site | Baikonur LC-1/5 | |||||||
| launch_contractor | ||||||||
| deployment_from | ||||||||
| deployment_date | ||||||||
| entered_service | ||||||||
| disposal_type | ||||||||
| deactivated | ||||||||
| destroyed | ||||||||
| last_contact | ||||||||
| recovery_by | ||||||||
| recovery_date | ||||||||
| decay_date | ||||||||
| landing_date | ||||||||
| landing_site | ||||||||
| {{end date | YYYY | MM | DD | hh | mm | ss | TZ | Z}} (for Zulu/UTC) or (if time unknown) |
| orbit_reference | Heliocentric | |||||||
| orbit_regime | ||||||||
| orbit_longitude | ||||||||
| orbit_slot | ||||||||
| orbit_semimajor | ||||||||
| orbit_eccentricity | ||||||||
| orbit_periapsis | 0.652 AU | |||||||
| orbit_apoapsis | 1.001 AU | |||||||
| orbit_inclination | 3.7° | |||||||
| orbit_period | 274 days | |||||||
| orbit_RAAN | ||||||||
| orbit_arg_periapsis | ||||||||
| orbit_mean_anomaly | ||||||||
| orbit_mean_motion | ||||||||
| orbit_repeat | ||||||||
| orbit_velocity | ||||||||
| orbit_epoch | ||||||||
| orbit_rev_number | ||||||||
| apsis | helion | |||||||
| interplanetary | ||||||||
| type | flyby | |||||||
| object | Venus | |||||||
| orbits | ||||||||
| component | ||||||||
| arrival_date | July 19, 1964 | |||||||
| departure_date | ||||||||
| location | ||||||||
| distance | 100000 km | |||||||
| sample_mass | ||||||||
| surface_EVAs | ||||||||
| surface_EVA_time | ||||||||
| periapsis | ||||||||
| apoapsis | ||||||||
| inclination | ||||||||
| apsis | ||||||||
| trans_band | ||||||||
| trans_frequency | ||||||||
| trans_bandwidth | ||||||||
| trans_capacity | ||||||||
| trans_coverage | ||||||||
| trans_TWTA | ||||||||
| trans_EIRP | ||||||||
| trans_HPBW | ||||||||
| programme | Zond | |||||||
| previous_mission | program started | |||||||
| next_mission | Zond 2 | |||||||
| insignia | ||||||||
| insignia_caption | ||||||||
| insignia_alt | ||||||||
| insignia_size |
1.1 m diameter
The following template should be used for ONE of the three above fields "end_of_mission", "decay" or "landing" if the spacecraft is no longer operational. If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered. (for Zulu/UTC) or (if time unknown)
If in doubt, leave it out--
Zond 1 was a spacecraft of the Soviet Zond program. It was the second Soviet research spacecraft to reach Venus, although communications had failed by that time. It carried a 90 cm spherical landing capsule, containing experiments for chemical analysis of the atmosphere, gamma-ray measurements of surface rocks, a photometer, temperature and pressure gauges, and a motion/rocking sensor in case it landed in water. An experimental Ion thruster was also carried for evaluation.
History
At least three previous Soviet planetary probes had been lost due to malfunctions of the ullage rockets (BOZ) on the Blok L stage, but an investigation found that the problem was easily resolved. The spacecraft, a Venera 3MV-1, was launched on April 2, 1964, from Tyuratam and this time the launch vehicle performed flawlessly. During the cruise phase, a slow leak from a cracked sensor window caused the electronics compartment to lose air pressure. This was a serious problem as Soviet electronics relied on vacuum tubes which would overheat without cooling air. An ill-timed command from ground control turned on its radio system while there was still a rarefied atmosphere inside, causing the electronics to short out by corona discharge. Chief Designer Sergei Korolev was upset at the failure of the mission and demanded higher quality control from the OKB-1 Bureau, including X-rays to test for pressure leaks.
By mid-April, the electronics in the main spacecraft had completely failed and all signal transmission ceased, but communication via the lander could still be performed, and space radiation and atomic-hydrogen spectrometer measurements were received. The experimental ion thruster-based attitude control system were also tested but found to operate erratically, possibly due to the loss of pressure in the electronics compartment. The star trackers in the spacecraft were also used to align it for a course-correction burn, but the second one was off by 65 feet per second (20 meters per second). Also one of the star trackers failed, forcing ground controllers to place Zond 1 into a spin-stabilization mode. However, all communications had failed by May 14. It passed 100,000 km from Venus on July 14, 1964.
A similar design of landing capsule was used in Venera 3.
Naming
Zond missions were presented as engineering tests by the Soviet Union and to an extent at least that may have been the case.
References
References
- (April 2, 2020). "Zond 1: The First Lander Sent to Venus".
- (2011). "Soviet Robots in the Solar System Mission Technologies and Discoveries". Springer-Praxis.
- Harvey, Brian. (2007). "Russian Planetary Exploration History, Development, Legacy and Prospects". Springer-Praxis.
This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.
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