|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:configuration
|
3-stage rocket
|
|
gptkbp:debut
|
over 30 launches
|
|
gptkbp:design_purpose
|
gptkb:scientific_research
gptkb:national_defense
satellite deployment
interplanetary missions
orbital insertion
|
|
gptkbp:development
|
gptkb:Long_March_3_family
|
|
gptkbp:diameter
|
3.35 meters
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:height
|
54 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Long March 3 B
|
|
gptkbp:launch_date
|
several per year
|
|
gptkbp:launch_platform
|
gptkb:Xichang_Satellite_Launch_Center
|
|
gptkbp:launch_price
|
approximately $50 million
|
|
gptkbp:launch_site
|
gptkb:Xichang_Satellite_Launch_Center
|
|
gptkbp:launched
|
gptkb:Beidou_satellites
gptkb:Chang'e_missions
gptkb:Tianwen-1_mission
|
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
|
gptkbp:mass
|
400,000 kg
|
|
gptkbp:notable_features
|
modular design
reusable components
high thrust
advanced guidance system
high payload capacity
multiple payload configurations
|
|
gptkbp:notable_launches
|
gptkb:China's_first_Mars_mission
gptkb:China's_first_lunar_probe
gptkb:Earth_observation
scientific satellites
multiple communication satellites
|
|
gptkbp:number_of_stages
|
gptkb:YF-24
gptkb:YF-25
YF-75
|
|
gptkbp:operated_by
|
gptkb:China_National_Space_Administration
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
2,500 kg
5,000 kg
11,000 kg to LEO
|
|
gptkbp:release_country
|
limited
|
|
gptkbp:reliability
|
high
|
|
gptkbp:success_rate
|
over 90%
|
|
gptkbp:successor
|
gptkb:Long_March_4_B
|
|
gptkbp:used_for
|
satellite launches
|
|
gptkbp:bfsParent
|
gptkb:Space_Launch_Complex_49
gptkb:Chang'e_3
gptkb:China_National_Space_Administration
gptkb:Xichang_Satellite_Launch_Center
gptkb:LE-5_B_engine
gptkb:Chinese_Satellite
|
|
gptkbp:bfsLayer
|
5
|