|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:configuration
|
stage-and-a-half
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
3.05 m
|
|
gptkbp:engine
|
gptkb:MA-2
|
|
gptkbp:family
|
gptkb:Titan
|
|
gptkbp:firstFlight
|
1957-06-11
|
|
gptkbp:firstICBMTest
|
1957
|
|
gptkbp:height
|
28.7 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Atlas rocket (legacy)
|
|
gptkbp:launchSite
|
gptkb:Cape_Canaveral
gptkb:Vandenberg_AFB
|
|
gptkbp:manufacturer
|
gptkb:Convair
|
|
gptkbp:mass
|
120,000 kg
|
|
gptkbp:notableFeature
|
balloon tank design
stage-and-a-half configuration
used for first American orbital crewed flight
|
|
gptkbp:notableMission
|
gptkb:Pioneer_10
gptkb:Mercury-Atlas_6
gptkb:Mariner_4
|
|
gptkbp:numberOfLaunches
|
over 500
|
|
gptkbp:numberOfStages
|
1.5
|
|
gptkbp:payload
|
gptkb:Friendship_7
gptkb:Pioneer_11
gptkb:Mariner_9
|
|
gptkbp:predecessor
|
nan
|
|
gptkbp:propulsion
|
gptkb:RP-1
liquid oxygen
|
|
gptkbp:retired
|
2004
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Atlas_II
|
|
gptkbp:successRate
|
~80%
|
|
gptkbp:usedBy
|
gptkb:NASA
gptkb:US_Air_Force
|
|
gptkbp:usedFor
|
gptkb:ICBM
space launch vehicle
|
|
gptkbp:usedIn
|
gptkb:Project_Mercury
gptkb:Gemini_program_(as_Atlas-Agena)
gptkb:Pioneer_program
gptkb:Mariner_program
|
|
gptkbp:bfsParent
|
gptkb:Lockheed_Martin
|
|
gptkbp:bfsLayer
|
5
|