Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designation |
G-26D
|
| gptkbp:developedBy |
1946–1957
|
| gptkbp:guidanceSystem |
inertial navigation
|
| https://www.w3.org/2000/01/rdf-schema#label |
G-26D Navaho
|
| gptkbp:influenced |
US rocket technology
|
| gptkbp:intendedRole |
intercontinental cruise missile
|
| gptkbp:length |
24.8 m
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:payload |
nuclear test
|
| gptkbp:propulsion |
rocket booster
ramjet |
| gptkbp:range |
about 5,500 km
|
| gptkbp:relatedTo |
gptkb:SM-64_Navaho
|
| gptkbp:status |
canceled
|
| gptkbp:successor |
ICBM programs
|
| gptkbp:testFlights |
1956–1958
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:wingspan |
12.2 m
|
| gptkbp:bfsParent |
gptkb:SM-64_Navaho_missile_program
|
| gptkbp:bfsLayer |
7
|