|
gptkbp:instance_of
|
gptkb:Space_Shuttle
|
|
gptkbp:analysis
|
ground-based analysis
|
|
gptkbp:collaboration
|
yes
|
|
gptkbp:collaborator
|
gptkb:Italian_Space_Agency
|
|
gptkbp:collection
|
plasma measurements
|
|
gptkbp:community_engagement
|
public demonstrations
|
|
gptkbp:community_outreach
|
STEM programs
|
|
gptkbp:data_transmission
|
gptkb:radio_station
|
|
gptkbp:developed_by
|
gptkb:NASA
|
|
gptkbp:elevation
|
approximately 300 kilometers
|
|
gptkbp:end_date
|
1996-07-31
|
|
gptkbp:first_flight
|
gptkb:1992
gptkb:1996
|
|
gptkbp:funding
|
NASA budget
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NASA's Tethered Satellite System program
|
|
gptkbp:impact
|
advancements in propulsion systems
|
|
gptkbp:key_concept
|
electrodynamic tethers
|
|
gptkbp:launch_date
|
1992-06-24
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Shuttle
|
|
gptkbp:legacy
|
influence on future tether missions
|
|
gptkbp:mission
|
successful
|
|
gptkbp:mission_duration
|
approximately 10 days
|
|
gptkbp:mission_type
|
technology demonstration
|
|
gptkbp:operational_status
|
completed
|
|
gptkbp:orbital_inclination
|
28.5 degrees
|
|
gptkbp:project
|
gptkb:Dr._John_W._Mc_Gowan
Tethered Aerostat Program
|
|
gptkbp:purpose
|
demonstrate tether technology
|
|
gptkbp:research_focus
|
spacecraft dynamics
|
|
gptkbp:route
|
20 kilometers
|
|
gptkbp:scientific_goals
|
study atmospheric phenomena
|
|
gptkbp:scientific_instruments
|
particle detectors
magnetometers
plasma wave instruments
|
|
gptkbp:successor
|
gptkb:Tethered_Satellite_System_2
|
|
gptkbp:tether_deployment_method
|
spooling
|
|
gptkbp:tether_material
|
kevlar
|
|
gptkbp:tether_retrieval_method
|
reeling
|
|
gptkbp:tethered_satellite
|
gptkb:Tethered_Satellite_System_1
gptkb:Tethered_Satellite_System_2
|
|
gptkbp:tethered_satellite_communication
|
radio signals
|
|
gptkbp:tethered_satellite_control
|
gptkb:ground
|
|
gptkbp:tethered_satellite_data
|
real-time data transmission
|
|
gptkbp:tethered_satellite_deployment
|
during orbit
|
|
gptkbp:tethered_satellite_design
|
modular design
|
|
gptkbp:tethered_satellite_experiment
|
electrodynamic propulsion study
plasma interaction study
tether dynamics study
|
|
gptkbp:tethered_satellite_function
|
gptkb:scientific_research
|
|
gptkbp:tethered_satellite_launch
|
gptkb:Space_Shuttle_Endeavour
|
|
gptkbp:tethered_satellite_mass
|
approximately 100 kg
|
|
gptkbp:tethered_satellite_mission
|
gptkb:Tethered_Satellite_System_1
gptkb:Tethered_Satellite_System_2
|
|
gptkbp:tethered_satellite_power
|
solar panels
|
|
gptkbp:tethered_satellite_retrieval
|
after mission completion
|
|
gptkbp:tethered_satellite_stability
|
active stabilization systems
|
|
gptkbp:tethered_satellite_system
|
gptkb:Tethered_Satellite_System_1
gptkb:Tethered_Satellite_System_2
|
|
gptkbp:bfsParent
|
gptkb:Tethered_Satellite_System-2
|
|
gptkbp:bfsLayer
|
5
|