Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:solid_rocket_motor
|
| gptkbp:alsoKnownAs |
X-248
|
| gptkbp:burnTime |
28 seconds
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.53 meters
|
| gptkbp:firstFlight |
1958
|
| gptkbp:length |
1.7 meters
|
| gptkbp:manufacturer |
gptkb:Thiokol
|
| gptkbp:mass |
264 kg
|
| gptkbp:propulsion |
gptkb:stone
|
| gptkbp:successor |
Altair 2 solid rocket motor
|
| gptkbp:thrust |
26.7 kN
|
| gptkbp:usedAs |
gptkb:upper_stage
kick stage |
| gptkbp:usedIn |
gptkb:Scout_rocket
gptkb:satellite gptkb:Vanguard_rocket |
| gptkbp:bfsParent |
gptkb:Thor-Able
gptkb:Thor-Delta gptkb:Thor-Delta_E1 gptkb:Thor-Delta_rocket |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Altair solid rocket motor
|