Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
suborbital launch vehicle
|
| gptkbp:alternativeName |
gptkb:OSP-L_II
|
| gptkbp:capacity |
up to 1,400 kg
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:Minuteman_II_ICBM
|
| gptkbp:diameter |
1.67 m
|
| gptkbp:family |
gptkb:Minotaur_rocket_family
|
| gptkbp:firstFlight |
1997
|
| https://www.w3.org/2000/01/rdf-schema#label |
Minotaur II
|
| gptkbp:launchSite |
gptkb:Vandenberg_Air_Force_Base
|
| gptkbp:length |
19.21 m
|
| gptkbp:manufacturer |
gptkb:Northrop_Grumman_Innovation_Systems
|
| gptkbp:mass |
36,200 kg
|
| gptkbp:numberOfStages |
3
|
| gptkbp:propulsion |
solid fuel
|
| gptkbp:purpose |
suborbital research and target vehicle
|
| gptkbp:stage2 |
SR19AJ1
|
| gptkbp:stage3 |
gptkb:SR73-AJ
|
| gptkbp:stageName |
gptkb:M55A1
|
| gptkbp:status |
active
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:bfsParent |
gptkb:RP-1
|
| gptkbp:bfsLayer |
5
|