|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Agena_series
|
|
gptkbp:communication
|
Telemetry
|
|
gptkbp:controls
|
gptkb:Reaction_Control_System
|
|
gptkbp:decommissioned
|
gptkb:1978
|
|
gptkbp:design
|
1 year
|
|
gptkbp:developer
|
$50 million
|
|
gptkbp:diameter
|
2.4 meters
|
|
gptkbp:durability
|
gptkb:battle
|
|
gptkbp:elevation
|
Low Earth Orbit
|
|
gptkbp:engine_type
|
Hypergolic
|
|
gptkbp:events
|
95%
|
|
gptkbp:first_flight
|
gptkb:television_series
1978-05-30
1960-04-08
|
|
gptkbp:fuel_type
|
Hydrazine
|
|
gptkbp:guidance_system
|
Inertial
|
|
gptkbp:height
|
3.6 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Agena X
|
|
gptkbp:launch_date
|
Monthly
|
|
gptkbp:launch_site
|
gptkb:cape
Remote
Ground
|
|
gptkbp:launch_vehicle
|
gptkb:Photographer
1,500 kg
|
|
gptkbp:launched
|
gptkb:television_series
Daytime
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
1,500 kg
|
|
gptkbp:mission
|
Polar Orbit
Reconnaissance
CORONA
|
|
gptkbp:mission_duration
|
6 months
|
|
gptkbp:operated_by
|
gptkb:aircraft
|
|
gptkbp:operational_area
|
1960-1978
|
|
gptkbp:propulsion
|
15 k N
|
|
gptkbp:purpose
|
gptkb:spacecraft
|
|
gptkbp:seating_capacity
|
gptkb:battle
gptkb:satellite
500 kg
1,000 kg
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:GEMINI
gptkb:Agena_D
|
|
gptkbp:track
|
Ground-based
|