Statements (60)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:communicationEquipment |
radio
|
| gptkbp:controls |
remote control
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:crew |
unmanned
|
| gptkbp:decommissioned |
1990s
|
| gptkbp:deployedTo |
military
|
| gptkbp:developedBy |
gptkb:Thomson-CSF
|
| gptkbp:endurance |
6 hours
|
| gptkbp:engineType |
piston engine
|
| gptkbp:exportedTo |
various countries
|
| gptkbp:features |
cost-effective
data encryption high endurance modular design real-time data transmission user-friendly interface multi-mission capability advanced avionics weather resistance high maneuverability low radar cross-section high altitude capability data storage capacity long-range communication autonomous flight integrated systems advanced telemetry quick deployment easy maintenance real-time video feed night vision capability high payload flexibility modular payloads multi-sensor capability stealth_technology |
| gptkbp:firstFlight |
1980
|
| https://www.w3.org/2000/01/rdf-schema#label |
Thomson-CSF Cyrano IV
|
| gptkbp:introduced |
1980
|
| gptkbp:launchSite |
catapult
|
| gptkbp:length |
3.5 meters
|
| gptkbp:manufacturer |
gptkb:Thomson-CSF
|
| gptkbp:maxSpeed |
200 km/h
|
| gptkbp:navigationEquipment |
gptkb:GPS
|
| gptkbp:operationalArea |
surveillance
|
| gptkbp:operationalStatus |
3000 meters
|
| gptkbp:payloadCapacity |
50 kg
|
| gptkbp:productionCompany |
1970s to 1980s
|
| gptkbp:range |
100 km
|
| gptkbp:relatedTo |
gptkb:Thomson-CSF
|
| gptkbp:renovated |
parachute
|
| gptkbp:role |
reconnaissance
|
| gptkbp:sensors |
optical
infrared radar |
| gptkbp:successor |
gptkb:Thomson-CSF_Cyrano_II
|
| gptkbp:type |
drone
|
| gptkbp:usedIn |
military operations
|
| gptkbp:weight |
200 kg
|
| gptkbp:wingspan |
4.5 meters
|