Properties (91)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:airlines |
up to 6 months
|
| gptkbp:communicationEquipment |
VHF radio
radio |
| gptkbp:controls |
automatic and manual
|
| gptkbp:coolingSystem |
ablative material
|
| gptkbp:crew |
simulator training
|
| gptkbp:crewCapacity |
3
launch escape system high priority safe return of astronauts safe_return_to_Earth |
| gptkbp:crewSize |
side-by-side seating
|
| gptkbp:currentUse |
transporting astronauts to ISS
|
| gptkbp:design |
gptkb:Soviet_Union
10 years conical_shape |
| gptkbp:designedBy |
gptkb:S.P._Korolev_Rocket_and_Space_Corporation_Energia
|
| gptkbp:designedFor |
human spaceflight
|
| gptkbp:diedIn |
environmental control system
closed-loop system |
| gptkbp:dimensions |
2.2 m diameter
|
| gptkbp:emergencyServices |
controlled descent
land or water detailed manual |
| gptkbp:environmentalImpact |
ablative heat shield
multi-layer insulation |
| gptkbp:features |
heat shield
|
| gptkbp:firstFlight |
gptkb:Soyuz_MS-19
gptkb:Soyuz_1 1967 |
| gptkbp:fuelType |
hypergolic propellants
|
| gptkbp:historicalSignificance |
first crewed spacecraft to return safely from orbit
first crewed spacecraft to return safely |
| https://www.w3.org/2000/01/rdf-schema#label |
Soyuz Descent Module
|
| gptkbp:inspiration |
future spacecraft designs
|
| gptkbp:internationalCooperation |
used by multiple countries
ISS missions NASA_and_ESA |
| gptkbp:isUpdatedBy |
2020
|
| gptkbp:landingGear |
parachute
designated landing area main and reserve parachutes at 10,000 m |
| gptkbp:launchDate |
over 140 missions
over 150 missions |
| gptkbp:launched |
approximately 5-10 per year
approximately 2-3 per year ground control team |
| gptkbp:launchSite |
Baikonur Cosmodrome
|
| gptkbp:launchVehicle |
gptkb:Soyuz_rocket
|
| gptkbp:manufacturer |
gptkb:RSC_Energia
|
| gptkbp:mission |
crew capsule
|
| gptkbp:missions |
onboard computer system
|
| gptkbp:modifications |
various upgrades over time
|
| gptkbp:navigationEquipment |
inertial navigation
|
| gptkbp:notableFeature |
gptkb:Kazakhstan
gptkb:Apollo-Soyuz_Test_Project Expedition missions to ISS International_Space_Station_missions |
| gptkbp:operatedBy |
gptkb:Russian_space_agency
|
| gptkbp:operationalStatus |
1967
in service currently operational low_Earth_orbit |
| gptkbp:partOf |
gptkb:Soyuz_spacecraft
|
| gptkbp:payloadCapacity |
up to 100 kg
|
| gptkbp:postRetirementCareer |
crew extraction and medical check
|
| gptkbp:productionYears |
over 50 years
|
| gptkbp:project |
periodic improvements
|
| gptkbp:renovated |
search and rescue team
water landing helicopter support land or water ground recovery team |
| gptkbp:respondsTo |
30 degrees
reentry capsule ballistic_trajectory |
| gptkbp:safetyFeatures |
redundant systems
multiple redundant systems high safety record |
| gptkbp:secondaryMission |
data collection and review
|
| gptkbp:services |
gptkb:Soyuz_Service_Module
|
| gptkbp:speed |
28,000 km/h
7.5 km/s |
| gptkbp:successor |
gptkb:Soyuz_MS_series
gptkb:Soyuz_MS |
| gptkbp:training |
cosmonaut training program
|
| gptkbp:usedBy |
gptkb:Russian_space_program
|
| gptkbp:usedFor |
human spaceflight
|
| gptkbp:weight |
2,500 kg
|