Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:rocket_motor
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.68 m (first stage)
|
| gptkbp:firstFlight |
1961
|
| gptkbp:length |
varies by stage
|
| gptkbp:manufacturer |
gptkb:Thiokol
gptkb:Aerojet gptkb:Hercules_Inc. |
| gptkbp:numberOfStages |
first stage
third stage second stage |
| gptkbp:propulsion |
solid fuel
|
| gptkbp:thrust |
~106 kN (third stage)
~267 kN (second stage) ~909 kN (first stage) |
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:usedFor |
gptkb:surface-to-air_missile
|
| gptkbp:usedIn |
gptkb:LGM-30_Minuteman
gptkb:Minuteman_III gptkb:Minuteman_II gptkb:Minuteman_I |
| gptkbp:bfsParent |
gptkb:Thiokol_Propulsion
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Minuteman missile motors
|