Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:Thor_missile
|
| gptkbp:diameter |
2.44 m
|
| gptkbp:failedLaunches |
2
|
| gptkbp:family |
gptkb:Delta_rocket_family
|
| gptkbp:firstFlight |
1960-05-13
|
| https://www.w3.org/2000/01/rdf-schema#label |
Thor-Delta rocket
|
| gptkbp:lastFlight |
1962-09-19
|
| gptkbp:launchSite |
gptkb:Cape_Canaveral_LC-17
gptkb:Vandenberg_AFB |
| gptkbp:length |
27.8 m
|
| gptkbp:manufacturer |
gptkb:Douglas_Aircraft_Company
|
| gptkbp:mass |
approx. 50,000 kg
|
| gptkbp:numberOfLaunches |
10
12 |
| gptkbp:numberOfStages |
gptkb:Delta_upper_stage
3 |
| gptkbp:payload |
gptkb:Explorer_12
gptkb:Echo_1A gptkb:TIROS-3 |
| gptkbp:payloadToGTO |
approx. 150 kg
|
| gptkbp:payloadToLEO |
approx. 450 kg
|
| gptkbp:predecessor |
gptkb:Thor-Able_rocket
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Delta_A
|
| gptkbp:thirdPlace |
gptkb:Altair_solid_rocket_motor
|
| gptkbp:usedFor |
satellite launches
|
| gptkbp:bfsParent |
gptkb:Rocket_Garden
|
| gptkbp:bfsLayer |
6
|