Statements (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:airlines |
lunar trajectory
|
| gptkbp:analyzes |
post-mission analysis
|
| gptkbp:communicationEquipment |
UHF radio
|
| gptkbp:controls |
ground control
autonomous guidance |
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:dataTransmission |
telemetry data
scientific data |
| gptkbp:dataUsage |
magnetic field measurements
cosmic ray data images of the Moon |
| gptkbp:dimensions |
2.4 m x 2.4 m x 2.4 m
|
| gptkbp:finalScore |
mission concluded
|
| gptkbp:financialPerformance |
study lunar surface
measure solar wind test spacecraft technologies |
| gptkbp:historicalSignificance |
first spacecraft to reach the Moon in the Zond series
|
| https://www.w3.org/2000/01/rdf-schema#label |
Zond 2
|
| gptkbp:launchDate |
1965-11-30
|
| gptkbp:launched |
gptkb:Soviet_Union
November 1965 |
| gptkbp:launchSite |
Baikonur Cosmodrome
1,200 kg |
| gptkbp:launchVehicle |
Molniya-M
|
| gptkbp:legacy |
paved the way for future lunar missions
|
| gptkbp:mission |
lunar flyby
|
| gptkbp:missions |
gptkb:Moscow
approximately 6 months |
| gptkbp:missionsConducted |
partially successful
|
| gptkbp:operationalStatus |
1965-1966
|
| gptkbp:orbitalInclination |
45 degrees
apoapsis of 1,000 km periapsis of 1,000 km |
| gptkbp:powers |
solar panels
|
| gptkbp:predecessor |
Zond_1
|
| gptkbp:relatedPatent |
gptkb:Zond_program
|
| gptkbp:researchInterest |
gptkb:Soviet_space_program
enhanced understanding of lunar environment provided data for future missions contributed to lunar exploration |
| gptkbp:respondsTo |
not designed for reentry
|
| gptkbp:scientificName |
magnetometer
cosmic ray detector television camera |
| gptkbp:secondaryMission |
1966-02-03
|
| gptkbp:status |
successfully completed mission
|
| gptkbp:successor |
gptkb:Zond_3
|
| gptkbp:weight |
1,200 kg
|