|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:derivedFrom
|
decommissioned Minuteman missiles
decommissioned Peacekeeper missiles
|
|
gptkbp:family
|
gptkb:Minotaur_family
|
|
gptkbp:firstFlight
|
2000
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Minotaur launch vehicles
|
|
gptkbp:launchSite
|
gptkb:Wallops_Flight_Facility
gptkb:Cape_Canaveral_Space_Force_Station
gptkb:Vandenberg_Space_Force_Base
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman_Innovation_Systems
|
|
gptkbp:market
|
government payloads
military payloads
small satellites
|
|
gptkbp:notableMission
|
gptkb:ORS-1
gptkb:TacSat-2
gptkb:TacSat-3
gptkb:LADEE
gptkb:TacSat-4
gptkb:STPSat-6
ORS-5
|
|
gptkbp:numberOfStages
|
4
5 (Minotaur V)
|
|
gptkbp:operator
|
gptkb:United_States_Air_Force
gptkb:United_States_Space_Force
|
|
gptkbp:payloadToLEO
|
1,735 kg (Minotaur IV)
580 kg (Minotaur I)
|
|
gptkbp:prohibits
|
not available for commercial launches due to US law
|
|
gptkbp:propulsion
|
solid fuel
|
|
gptkbp:relatedTo
|
gptkb:Minuteman_missile
gptkb:Peacekeeper_missile
Pegasus launch vehicle
Taurus launch vehicle
|
|
gptkbp:status
|
active
|
|
gptkbp:successRate
|
high
|
|
gptkbp:usedFor
|
orbital launches
suborbital launches
|
|
gptkbp:variant
|
gptkb:Minotaur_I
gptkb:Minotaur_II
gptkb:Minotaur_III
gptkb:Minotaur_IV
gptkb:Minotaur_V
gptkb:Minotaur_VI
|
|
gptkbp:website
|
https://www.northropgrumman.com/space/minotaur-launch-vehicle/
|
|
gptkbp:bfsParent
|
gptkb:decommissioned_Minuteman_and_Peacekeeper_ICBMs
|
|
gptkbp:bfsLayer
|
7
|