Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:book |
Minuteman II SR19
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:Minuteman_II_missile
gptkb:Pegasus_rocket |
| gptkbp:diameter |
1.67 meters
|
| gptkbp:firstFlight |
2000-01-27
|
| gptkbp:fourthGenerationYears |
gptkb:Orion_38
|
| gptkbp:height |
19.21 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Minotaur I rocket
|
| gptkbp:launchSite |
gptkb:Vandenberg_Air_Force_Base
gptkb:Wallops_Flight_Facility |
| gptkbp:manufacturer |
gptkb:Northrop_Grumman_Innovation_Systems
|
| gptkbp:mass |
36,200 kg
|
| gptkbp:numberOfLaunches |
12
|
| gptkbp:numberOfStages |
4
Minuteman II M55A1 |
| gptkbp:operator |
gptkb:United_States_Air_Force
gptkb:Northrop_Grumman |
| gptkbp:payloadToLEO |
580 kg
|
| gptkbp:propulsion |
solid fuel
|
| gptkbp:status |
active
|
| gptkbp:thirdPlace |
gptkb:Orion_50XL
|
| gptkbp:usedFor |
launching small satellites
|
| gptkbp:website |
https://www.northropgrumman.com/space/minotaur-launch-vehicles/
|
| gptkbp:bfsParent |
gptkb:Orion_50XL
|
| gptkbp:bfsLayer |
7
|