|
gptkbp:instance_of
|
gptkb:spacecraft
gptkb:rocket
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:State_Corporation_for_Activities_in_Space
|
|
gptkbp:aircraft_operated
|
gptkb:beer
|
|
gptkbp:challenges
|
overcame early design issues
|
|
gptkbp:collaborated_with
|
other Soviet space agencies
|
|
gptkbp:collaborations
|
limited
|
|
gptkbp:communication
|
gptkb:radio_station
|
|
gptkbp:controls
|
inertial navigation
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Valery_Ryumin
gptkb:Alexander_Aleksandrov
gptkb:3
gptkb:Viktor_Savinykh
gptkb:Sergei_Avdeyev
gptkb:Viktor_Afanasyev
gptkb:Thomas_Reiter
required
|
|
gptkbp:date
|
1997-03-22
|
|
gptkbp:decommissioned
|
after 1980
|
|
gptkbp:design
|
based on earlier Soyuz models
|
|
gptkbp:developed_by
|
gptkb:Monarch
|
|
gptkbp:developer
|
3 years
|
|
gptkbp:diameter
|
2.7 meters
10.3 m
|
|
gptkbp:duration
|
7 days
90 days
|
|
gptkbp:elevation
|
200 km
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
gptkb:1977
gptkb:Soyuz_25
gptkb:Soyuz_34
conducted before crewed missions
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
automatic and manual
|
|
gptkbp:height
|
49.5 m
|
|
gptkbp:historical_impact
|
significant in space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz-77
|
|
gptkbp:influenced
|
future Soyuz designs
|
|
gptkbp:influenced_by
|
gptkb:Vostok_program
|
|
gptkbp:inspiration
|
for future space vehicles
|
|
gptkbp:is_a_destination_for
|
gptkb:Mir
|
|
gptkbp:is_involved_in
|
space station missions
|
|
gptkbp:is_used_for
|
gptkb:Research_Institute
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
1996-12-20
1980-11-26
1982-11-26
1977-11-26
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz
gptkb:Soyuz-U
gptkb:spacecraft
3000 kg
|
|
gptkbp:launched
|
gptkb:musical
gptkb:10
|
|
gptkbp:legacy
|
paved the way for future missions
|
|
gptkbp:length
|
7.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Korolev_Rocket_and_Space_Corporation
gptkb:Monarch
|
|
gptkbp:mass
|
2800 kg
|
|
gptkbp:mission
|
gptkb:Salyut_7
completed
successful
crewed
|
|
gptkbp:mission_duration
|
7 days
90 days
up to 30 days
168 hours
|
|
gptkbp:modifications
|
made during operational life
|
|
gptkbp:module
|
gptkb:Soyuz_TM
|
|
gptkbp:number_of_stages
|
gptkb:RD-107
gptkb:RD-108
gptkb:3
2
RD-0110
|
|
gptkbp:operational_area
|
1977-1980
|
|
gptkbp:operator
|
gptkb:Russian_Federal_Space_Agency
gptkb:Soviet_space_program
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:outcome
|
successful
|
|
gptkbp:part_of
|
Soviet space program history
|
|
gptkbp:predecessor
|
gptkb:Soyuz-76
gptkb:Soyuz_TM-24
|
|
gptkbp:project
|
gptkb:Vladimir_Chelomey
|
|
gptkbp:propulsion
|
gptkb:Soyuz_TM-25
100 k N
|
|
gptkbp:purpose
|
manned spaceflight
|
|
gptkbp:replaced_by
|
gptkb:Soyuz-79
|
|
gptkbp:retired
|
gptkb:1980
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:scholarships
|
included
|
|
gptkbp:seating_capacity
|
7,000 kg
500 kg to LEO
|
|
gptkbp:services
|
included
|
|
gptkbp:significance
|
part of Soviet space program
|
|
gptkbp:successor
|
gptkb:Soyuz-78
gptkb:Soyuz-79
gptkb:Soyuz-T
gptkb:Soyuz_TM-25
|