|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Gaofen_series
gptkb:Space_Launch_Complex_49
|
|
gptkbp:debut_year
|
over 30 launches
|
|
gptkbp:design
|
gptkb:satellite
|
|
gptkbp:developer
|
ongoing
|
|
gptkbp:diameter
|
3.35 meters
|
|
gptkbp:engine
|
two YF-21 engines
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:events
|
over 90% success rate
|
|
gptkbp:first_flight
|
December 30, 2006
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
gptkbp:guidance_system
|
inertial guidance
|
|
gptkbp:height
|
43.1 meters
|
|
gptkbp:historical_event
|
derived from Long March 4 B
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Long March 4 C
|
|
gptkbp:is_used_for
|
satellite launches
|
|
gptkbp:launch_date
|
frequent
|
|
gptkbp:launch_site
|
gptkb:Taiyuan_Satellite_Launch_Center
automated
|
|
gptkbp:launch_vehicle
|
gptkb:Long_March_4
modular design
satellite deployment
expendable launch vehicle
medium-lift
245,000 kg
|
|
gptkbp:launched
|
multiple satellites
|
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
|
gptkbp:market
|
approximately $10 million
|
|
gptkbp:notable_album
|
gptkb:Gaofen_series_satellites
|
|
gptkbp:notable_features
|
high payload capacity
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_area
|
civil and commercial missions
|
|
gptkbp:operational_status
|
gptkb:2006
active
|
|
gptkbp:origin
|
gptkb:China
|
|
gptkbp:primary_user
|
gptkb:China_National_Space_Administration
|
|
gptkbp:propulsion
|
1,200 k N
|
|
gptkbp:release_region
|
limited
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:seating_capacity
|
1,200 kg
2,500 kg
4 meters in diameter
various satellite types
|
|
gptkbp:setting
|
two-stage
|
|
gptkbp:succeeded_by
|
high
|
|
gptkbp:upgrades
|
planned
|