|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:aircraft_operated
|
up to 30 days
|
|
gptkbp:capacity
|
up to 4 crew members
|
|
gptkbp:cargo_types
|
planned for future missions
|
|
gptkbp:challenges
|
overcoming new technologies
|
|
gptkbp:collaboration
|
ESA and NASA
|
|
gptkbp:collaborations
|
for research and development
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:launch_escape_system
high priority
integrated system
designed for human spaceflight
conducted at Gagarin Cosmonaut Training Center
|
|
gptkbp:design
|
completed
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:designed_by
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:development
|
gptkb:2010
|
|
gptkbp:durability
|
gptkb:true
|
|
gptkbp:emergency_services
|
land on land or water
|
|
gptkbp:environmental_impact
|
considered in design
|
|
gptkbp:facilities
|
gptkb:Gromov_Flight_Research_Institute
|
|
gptkbp:first_flight
|
gptkb:2023
planned for 2024
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:height
|
approximately 3.5 m
|
|
gptkbp:historical_significance
|
part of Russia's space legacy
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Oryol spacecraft
|
|
gptkbp:inspiration
|
gptkb:spacecraft
|
|
gptkbp:integration
|
6 months
|
|
gptkbp:is_a_supporter_of
|
planned for 2025
|
|
gptkbp:is_designed_to
|
lunar missions
future lunar missions
|
|
gptkbp:is_tested_for
|
ongoing
|
|
gptkbp:landing_distance
|
gptkb:parachute
|
|
gptkbp:launch_date
|
2025
annual
|
|
gptkbp:launch_price
|
estimated at $100 million
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-5
|
|
gptkbp:length
|
approximately 9.5 m
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mass
|
approximately 14,000 kg
|
|
gptkbp:mission
|
gptkb:Moscow_Mission_Control_Center
lunar missions planned
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_use
|
15 years
|
|
gptkbp:orbit_type
|
low Earth orbit
|
|
gptkbp:partnerships
|
with private space companies
|
|
gptkbp:payload_capacity
|
up to 500 kg
|
|
gptkbp:potential_commercial_use
|
for space tourism.
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:project
|
to be tested during missions
|
|
gptkbp:projected_upgrades
|
for future missions
|
|
gptkbp:public_interest
|
high due to lunar exploration plans
|
|
gptkbp:purpose
|
gptkb:human_spaceflight
|
|
gptkbp:recovery_method
|
separate from service module
|
|
gptkbp:regulatory_compliance
|
compliance required
|
|
gptkbp:research_opportunities
|
for scientific experiments
|
|
gptkbp:safety_features
|
radiation shielding
|
|
gptkbp:safety_rating
|
5-star
|
|
gptkbp:space_debris_mitigation
|
strategies in place
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:successor
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:support
|
gptkb:International_Space_Station
|
|
gptkbp:width
|
approximately 4.5 m
|
|
gptkbp:bfsParent
|
gptkb:Russian_Federal_Space_Agency_(Roscosmos)
gptkb:Soyuz_spacecraft
gptkb:Roscosmos
|
|
gptkbp:bfsLayer
|
4
|