Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:family |
gptkb:Atlas_rocket_family
|
| gptkbp:firstFlight |
1991-12-07
|
| gptkbp:height |
47.54 m
|
| gptkbp:lastFlight |
2004-08-31
|
| gptkbp:launchSite |
gptkb:Cape_Canaveral_Space_Launch_Complex_36
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:mass |
204,300 kg
|
| gptkbp:notableMission |
gptkb:Milstar_satellites
gptkb:GOES_satellites gptkb:TDRS_satellites |
| gptkbp:numberOfLaunches |
63
|
| gptkbp:numberOfStages |
gptkb:Dragon
2 |
| gptkbp:payloadToGTO |
3,810 kg
|
| gptkbp:payloadToLEO |
8,200 kg
|
| gptkbp:precededBy |
gptkb:Atlas_I
|
| gptkbp:propulsion |
RP-1/LOX
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Atlas_III
|
| gptkbp:successRate |
0%
|
| gptkbp:usedFor |
commercial payloads
launching satellites military payloads |
| gptkbp:variant |
gptkb:Atlas_IIA
gptkb:Atlas_IIAS gptkb:Atlas_II |
| gptkbp:bfsParent |
gptkb:RS-56_rocket_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Atlas II launch vehicle
|