|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:aircraft_operated
|
30 minutes
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew_capacity
|
gptkb:none
|
|
gptkbp:design_purpose
|
commercial satellite launches
|
|
gptkbp:development_cost
|
$200 million
|
|
gptkbp:diameter
|
3.5 meters
|
|
gptkbp:durability
|
partially reusable
|
|
gptkbp:engine
|
gas-generator cycle
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
2022-01-15
successful
|
|
gptkbp:guidance_system
|
GPS guidance
|
|
gptkbp:height
|
30 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
LC-82 B
|
|
gptkbp:launch_date
|
monthly
|
|
gptkbp:launch_frequency_per_year
|
gptkb:12
|
|
gptkbp:launch_platform
|
gptkb:remote_control
gptkb:NASA
|
|
gptkbp:launch_price
|
$10 million
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
expendable
LC series
Pad 39 A
|
|
gptkbp:launch_window
|
2 hours
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
95%
|
|
gptkbp:mission_type
|
gptkb:scientific_research
|
|
gptkbp:number_of_stages
|
2
1 engine
4 engines
|
|
gptkbp:operational_since
|
gptkb:2022
|
|
gptkbp:orbital_inclination
|
30 degrees
|
|
gptkbp:payload_capacity
|
5 meters
500 kg to Low Earth Orbit
600 kg to Geostationary Transfer Orbit
|
|
gptkbp:payload_interface
|
standard interface
|
|
gptkbp:primary_mission
|
satellite deployment
|
|
gptkbp:propulsion
|
RP-1 and Liquid Oxygen
150 k N
150 k N per engine
|
|
gptkbp:recovery_method
|
gptkb:none
|
|
gptkbp:status
|
active
|
|
gptkbp:bfsParent
|
gptkb:NIKKOR_Z_24-70mm_f/2.8_S
|
|
gptkbp:bfsLayer
|
7
|