National Aeronautics and Space Administration Logo
Follow this link to skip to the main content NASA Banner
Solar System Exploration
Missions
Zond 1
Missions to Venus
 By Target   By Name   By Decade 
Beyond Our Solar System Our Solar System Sun Mercury Venus Moon Earth Mars Dwarf Planets Dwarf Planets Dwarf Planets Asteroids Comets Jupiter Saturn Uranus Neptune Kuiper Belt
 
 Past 
 Present 
 Future 
 Concepts 
Zond 01
Zond 1 Mission to Venus

Mission Type: Lander
Launch Vehicle: Modified SS-6 (Sapwood) 8K78 (no. T15000-23)
Launch Site: Tyuratam (Baikonur Cosmodrome), U.S.S.R., NIIP-5 / launch site 1
Spacecraft Mass: 948 kg
Spacecraft Instruments:
Bus: 1) radiation detector; 2) charged-particle detector; 3) magnetometer; 4) piezoelectric detector and 5) atomic hydrogen detector
Lander:1) barometer; 2) thermometer; 3) radiation detector; 4) micro-organism detection experiment; 5) atmospheric composition experiment; 6) acidity measurement experiment; 7) electro-conductivity experiment and 8) luminosity experiment
References:
Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958-2000, Monographs in Aerospace History No. 24, by Asif A. Siddiqi

National Space Science Data Center, http://nssdc.gsfc.nasa.gov/


Although this Venus impact probe was successfully sent toward Venus, ground controllers discovered a series of major malfunctions in the spacecraft during its coast to the planet. These included depressurization of the main spacecraft bus when the glass cover of a solar-stellar attitude-control sensor cracked. Additionally, the internal radio transmitters of the spacecraft were automatically switched on at the wrong time -- during depressurization, when the gas discharge created high-voltage currents that shorted out the system.

Contact was maintained with the still-pressurized 290-kilogram lander module until 25 May 1964, by which time controllers had managed to conduct two major course corrections (at 560,000 kilometers and 13 to 14 million kilometers from Earth, respectively), the first time such actions had been performed on a Soviet interplanetary spacecraft.

The inert spacecraft eventually flew by Venus on 19 July 1964 at a range of 110,000 kilometers. The Soviets later published some data on cosmic-ray flux measured by Zond 1.


Key Dates
2 Apr 1964:  Launch
25 May 1964:  Contact Lost
19 Jul 1964:  Venus Flyby
Status: Partial Success
Fast Facts
Zond 01 Facts This was the first course corrections performed on a Soviet interplanetary spacecraft.

The spacecraft ended up in an heliocentric (Sun-centered) orbit.

Zond means probe in Russian.
Headlines
Links
Awards and Recognition   Solar System Exploration Roadmap   Contact Us   Site Map   Print This Page
NASA Official: Kristen Erickson
Advisory: Dr. James Green, Director of Planetary Science
Outreach Manager: Alice Wessen
Curator/Editor: Phil Davis
Science Writer: Autumn Burdick
Producer: Greg Baerg
Webmaster: David Martin
> NASA Science Mission Directorate
> Budgets, Strategic Plans and Accountability Reports
> Equal Employment Opportunity Data
   Posted Pursuant to the No Fear Act
> Information-Dissemination Policies and Inventories
> Freedom of Information Act
> Privacy Policy & Important Notices
> Inspector General Hotline
> Office of the Inspector General
> NASA Communications Policy
> USA.gov
> ExpectMore.gov
> NASA Advisory Council
> Open Government at NASA
Last Updated: 2 Dec 2010