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gptkbp:instance_of
|
gptkb:missile
|
|
gptkbp:capacity
|
100 passengers
|
|
gptkbp:crew
|
gptkb:none
|
|
gptkbp:deployment
|
strategic deterrence
|
|
gptkbp:design
|
Vladimir Petrov
|
|
gptkbp:design_purpose
|
strategic nuclear strike
|
|
gptkbp:designed_by
|
gptkb:Soviet_Union
gptkb:Royal_Aircraft_Establishment
|
|
gptkbp:developed_by
|
gptkb:United_Kingdom
|
|
gptkbp:development
|
gptkb:1975
gptkb:1980
|
|
gptkbp:diameter
|
1.5 meters
78 feet
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:fate
|
scrapped
|
|
gptkbp:first_flight
|
gptkb:1929
gptkb:1980
August 1929
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:guidance_system
|
gptkb:100_meters
inertial guidance
|
|
gptkbp:has_programs
|
Soviet missile program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-100 missile
|
|
gptkbp:initial_deployment_year
|
gptkb:1981
|
|
gptkbp:is_targeted_at
|
satellite guidance
|
|
gptkbp:is_tested_for
|
gptkb:10
gptkb:Kapustin_Yar
|
|
gptkbp:launch_date
|
30 minutes
|
|
gptkbp:launch_platform
|
mobile launcher
automated system
|
|
gptkbp:launch_site
|
gptkb:Siberia
|
|
gptkbp:launched
|
45 degrees
Cardington Airship Shed
|
|
gptkbp:length
|
15 meters
777 feet
|
|
gptkbp:manufacturer
|
Moscow Engineering Institute
|
|
gptkbp:max_speed
|
84 mph
|
|
gptkbp:military_branch
|
gptkb:Strategic_Rocket_Forces
|
|
gptkbp:modifications
|
R-100 A
|
|
gptkbp:operated_by
|
gptkb:British_Air_Ministry
|
|
gptkbp:operational_use
|
gptkb:1981
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:payload_capacity
|
1000 kg
|
|
gptkbp:propulsion
|
liquid fuel
150 k N
|
|
gptkbp:range
|
5000 km
7,000 miles
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retirement
|
technological obsolescence
|
|
gptkbp:retirement_year
|
gptkb:1995
|
|
gptkbp:service_history
|
gptkb:Soviet_Armed_Forces
|
|
gptkbp:status
|
retired
|
|
gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:succeeded_by
|
R-101
|
|
gptkbp:success_rate
|
90%
|
|
gptkbp:successor
|
gptkb:R-200_missile
|
|
gptkbp:treaty
|
gptkb:START_I
|
|
gptkbp:type
|
gptkb:aircraft
gptkb:missile
|
|
gptkbp:used_for
|
passenger transport
|
|
gptkbp:warhead_type
|
nuclear
|
|
gptkbp:weight
|
8000 kg
|