Statements (64)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:spacecraft
|
| gptkbp:academic_programs |
comprised of top engineers
|
| gptkbp:challenges |
overcame numerous engineering challenges
|
| gptkbp:collaboration |
joint missions with other countries
|
| gptkbp:communication_system |
gptkb:radio_station
|
| gptkbp:control_system |
gptkb:navigation_system
|
| gptkbp:cooling_system |
ablative heat shield
|
| gptkbp:crew |
gptkb:launch_escape_system
2 emphasis on crew safety protocols extensive training required provided valuable experience for astronauts |
| gptkbp:crew_capacity |
gptkb:3
|
| gptkbp:cultural_impact |
featured in documentaries and films
|
| gptkbp:design_features |
modular design for easy maintenance
|
| gptkbp:design_philosophy |
focus on reliability and safety
|
| gptkbp:diameter |
2.2 meters
|
| gptkbp:educational_value |
used in educational programs
|
| gptkbp:first_flight |
1977-04-05
1976-11-20 |
| gptkbp:flight_style |
2
|
| gptkbp:funding |
funded by government and private sectors
|
| gptkbp:future_prospects |
influenced future space exploration missions
|
| gptkbp:has_ability |
considered a successful spacecraft
|
| gptkbp:has_documentation |
extensive technical documentation available
|
| gptkbp:historical_significance |
part of the Soviet space program
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soyuz 20 K-2
|
| gptkbp:innovation |
introduced several technical innovations
|
| gptkbp:inspiration |
inspired future generations of astronauts
|
| gptkbp:landing_site |
gptkb:Kazakhstan
|
| gptkbp:launch_date |
1976-11-20
launched multiple times |
| gptkbp:launch_event |
high launch success rate
|
| gptkbp:launch_mass |
7000 kg
|
| gptkbp:launch_site |
gptkb:Baikonur_Cosmodrome
|
| gptkbp:launch_vehicle |
gptkb:Soyuz_spacecraft
|
| gptkbp:legacy |
influenced future spacecraft designs
|
| gptkbp:length |
7.2 meters
|
| gptkbp:life_support_system |
closed-loop system
|
| gptkbp:manufacturer |
gptkb:Soviet_Union
|
| gptkbp:mass |
6800 kg
|
| gptkbp:mission |
successful return to Earth
varied mission objectives thorough post-mission analysis conducted |
| gptkbp:mission_duration |
7 days
|
| gptkbp:mission_type |
gptkb:human_spaceflight
|
| gptkbp:notable_mission |
gptkb:Salyut_7
|
| gptkbp:operational_history |
part of a long operational history
|
| gptkbp:operational_period |
1976-1977
|
| gptkbp:operational_use |
used for missions to space stations
|
| gptkbp:orbital_period |
90 minutes
|
| gptkbp:payload_capacity |
250 kg
|
| gptkbp:power_source |
solar panels
|
| gptkbp:public_interest |
generated significant public interest
|
| gptkbp:recovery_method |
gptkb:parachute
|
| gptkbp:retirement |
superseded by newer models
|
| gptkbp:safety_record |
high safety standards
|
| gptkbp:scientific_instruments |
various experiments
|
| gptkbp:spacecraft |
designed for long-duration missions
part of the Soyuz family of spacecraft |
| gptkbp:specification |
detailed engineering documents available
|
| gptkbp:speed |
ballistic reentry
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Soyuz_T
|