Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:V-2_rocket
|
| gptkbp:diameter |
1.78 m
|
| gptkbp:engine |
gptkb:Redstone_A-7_rocket_engine
|
| gptkbp:enteredService |
1958
|
| gptkbp:guidanceSystem |
inertial guidance
|
| https://www.w3.org/2000/01/rdf-schema#label |
BGM-8 Redstone
|
| gptkbp:launchWeight |
27,200 kg
|
| gptkbp:length |
21.8 m
|
| gptkbp:manufacturer |
gptkb:Chrysler
|
| gptkbp:nickname |
gptkb:Redstone
|
| gptkbp:platform |
mobile transporter erector launcher
|
| gptkbp:propulsion |
liquid-fueled
|
| gptkbp:range |
370 km
|
| gptkbp:retired |
1964
|
| gptkbp:usedBy |
gptkb:United_States_Army
|
| gptkbp:usedIn |
Project Mercury (as launch vehicle)
|
| gptkbp:warheadType |
gptkb:W39_nuclear_warhead
|
| gptkbp:warheadYield |
3.8 megatons
|
| gptkbp:bfsParent |
gptkb:Cold_War_weapons_of_the_United_States
|
| gptkbp:bfsLayer |
8
|