|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:control_system
|
inertial navigation
|
|
gptkbp:debut
|
gptkb:1959
gptkb:1976
|
|
gptkbp:designed_by
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
2.5 m
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:guidance_system
|
autonomous guidance
|
|
gptkbp:has_programs
|
gptkb:Luna_program
|
|
gptkbp:has_tour
|
two-stage rocket
|
|
gptkbp:height
|
23.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Luna rocket
|
|
gptkbp:last_successful_mission
|
gptkb:Luna_24
|
|
gptkbp:launch_event
|
85%
|
|
gptkbp:launch_platform
|
ground launch
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
expendable launch vehicle
Luna family
|
|
gptkbp:launched
|
gptkb:20
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mass
|
around 30,000 kg
|
|
gptkbp:mission
|
gptkb:Luna_2
|
|
gptkbp:notable_feature
|
first human-made object to reach the Moon
first sample return mission from the Moon
first spacecraft to achieve a soft landing on the Moon
first spacecraft to transmit images from the Moon's surface
|
|
gptkbp:notable_mission
|
gptkb:Luna_2
gptkb:Luna_9
gptkb:Luna_24
gptkb:Luna_16
|
|
gptkbp:operational_period
|
1959-1976
|
|
gptkbp:payload_capacity
|
gptkb:scientific_instruments
gptkb:lunar_landers
gptkb:lunar_rovers
up to 1,000 kg
sample return capsules
|
|
gptkbp:purpose
|
gptkb:Moon
|
|
gptkbp:successor
|
gptkb:Luna_16
|
|
gptkbp:type
|
gptkb:Space_Launch_System
|
|
gptkbp:used_for
|
sample return missions
lunar orbiters
hard landings on the Moon
soft landings on the Moon
|
|
gptkbp:bfsParent
|
gptkb:Luna_program
|
|
gptkbp:bfsLayer
|
4
|