Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:duration |
7 years
|
| gptkbp:launchDate |
2003-05-09
|
| gptkbp:launchSite |
gptkb:Uchinoura_Space_Center
|
| gptkbp:launchVehicle |
gptkb:M-V_rocket
|
| gptkbp:mass |
510 kg
|
| gptkbp:missionChallenges |
communication loss
fuel leak reaction wheel failures |
| gptkbp:missionType |
asteroid sample-return
|
| gptkbp:nameMeaning |
gptkb:Peregrine_Falcon
|
| gptkbp:notableAchievement |
first spacecraft to return asteroid samples to Earth
|
| gptkbp:operator |
gptkb:JAXA
|
| gptkbp:powers |
1.1 kW
|
| gptkbp:reentryDate |
gptkb:Woomera,_Australia
|
| gptkbp:returnedToEarth |
2010-06-13
|
| gptkbp:sampleReturned |
asteroid regolith
|
| gptkbp:status |
mission completed
|
| gptkbp:successor |
gptkb:Hayabusa2
|
| gptkbp:target |
gptkb:asteroid_25143_Itokawa
|
| gptkbp:website |
https://www.jaxa.jp/projects/sat/muses_c/index_e.html
|
| gptkbp:bfsParent |
gptkb:JAXA
gptkb:OSIRIS-REx_mission |
| gptkbp:bfsLayer |
5
|
| https://www.w3.org/2000/01/rdf-schema#label |
Hayabusa
|