Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
solid rocket motor
|
| gptkbp:alsoKnownAs |
gptkb:TE-M-711
|
| gptkbp:burnTime |
84 seconds
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.24 m
|
| gptkbp:firstFlight |
1982
|
| https://www.w3.org/2000/01/rdf-schema#label |
Star-48
|
| gptkbp:length |
2.08 m
|
| gptkbp:manufacturer |
gptkb:Thiokol
|
| gptkbp:mass |
2,011 kg
|
| gptkbp:propulsion |
gptkb:stone
|
| gptkbp:successor |
gptkb:Star-63
|
| gptkbp:thrust |
68.6 kN
|
| gptkbp:usedFor |
interplanetary missions
satellite deployment upper stage propulsion geostationary transfer orbit |
| gptkbp:usedIn |
gptkb:Space_Shuttle
gptkb:Delta_II_rocket gptkb:Atlas_II_rocket gptkb:Payload_Assist_Module_(PAM) |
| gptkbp:bfsParent |
gptkb:Atlas_H
|
| gptkbp:bfsLayer |
7
|