gptkbp:instanceOf
|
rocket
|
gptkbp:associatedWith
|
NASA
|
gptkbp:controls
|
pitch and yaw control
|
gptkbp:designedBy
|
gptkb:Wernher_von_Braun
|
gptkbp:diameter
|
5.5 feet
|
gptkbp:engineType
|
liquid-fueled engine
|
gptkbp:firstAwarded
|
gptkb:Juno_I
1960
|
gptkbp:firstFlight
|
1956-10-29
|
gptkbp:firstMatch
|
gptkb:Juno_II
|
gptkbp:gameFeatures
|
liquid oxygen and RP-1
|
https://www.w3.org/2000/01/rdf-schema#label
|
Jupiter C rocket
|
gptkbp:influenced
|
future rocket designs
|
gptkbp:influencedBy
|
German_rocket_technology
|
gptkbp:inspiration
|
V-2 rocket
|
gptkbp:involved
|
satellite technology
space science
Vanguard 1
aerospace education
reentry technology
|
gptkbp:involvedIn
|
gptkb:Project_Vanguard
space exploration
scientific payloads
radiation measurements
scientific research missions
rocket propulsion technology
international space research
|
gptkbp:launchDate
|
multiple test flights
|
gptkbp:launched
|
10
1956
|
gptkbp:launchSite
|
gptkb:Cape_Canaveral
5,500 kg
|
gptkbp:launchVehicle
|
sounding rocket
|
gptkbp:length
|
23.5 feet
|
gptkbp:manufacturer
|
Redstone Arsenal
|
gptkbp:maximumDepth
|
1,000 miles
|
gptkbp:nationalTeam
|
gptkb:United_States
|
gptkbp:notableEvent
|
first successful launch of a satellite by the US
|
gptkbp:notableFeature
|
Explorer 1
|
gptkbp:numberOfStudents
|
2
|
gptkbp:operatedBy
|
gptkb:Army_Ballistic_Missile_Agency
|
gptkbp:operationalStatus
|
retired
|
gptkbp:payloadCapacity
|
1,000 pounds
|
gptkbp:productionCompany
|
1950s
|
gptkbp:provides
|
inertial guidance
|
gptkbp:purpose
|
suborbital test flights
|
gptkbp:relatedTo
|
Jupiter_program
|
gptkbp:retired
|
1960s
|
gptkbp:significance
|
first_American_satellite_launch_vehicle
|
gptkbp:successor
|
Explorer_program
Jupiter_rocket
|
gptkbp:supports
|
upper atmosphere studies
|
gptkbp:usedBy
|
gptkb:United_States
|
gptkbp:usedFor
|
atmospheric research
|
gptkbp:weight
|
12,000 pounds
|