|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:airlines
|
15 minutes
|
|
gptkbp:collection
|
atmospheric_data
|
|
gptkbp:communicationEquipment
|
radio telemetry
|
|
gptkbp:controls
|
autonomous
|
|
gptkbp:crewCapacity
|
none
|
|
gptkbp:design
|
technology demonstration
|
|
gptkbp:diameter
|
1 meter
|
|
gptkbp:engineConfiguration
|
single engine
|
|
gptkbp:engineType
|
liquid propulsion
|
|
gptkbp:environmentalImpact
|
conducted
|
|
gptkbp:firstAwarded
|
liquid fuel engine
|
|
gptkbp:firstFlight
|
yes
|
|
gptkbp:firstGeneration
|
yes
|
|
gptkbp:firstMatch
|
solid fuel engine
|
|
gptkbp:fuelType
|
kerosene and liquid oxygen
|
|
gptkbp:futurePlans
|
further development
|
|
gptkbp:hasVersion
|
Kavoshgar-16
Kavoshgar-18
|
|
gptkbp:height
|
10 meters
|
|
gptkbp:homeGround
|
available
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kavoshgar-17
|
|
gptkbp:internationalCooperation
|
none
|
|
gptkbp:launchDate
|
2017-02-02
|
|
gptkbp:launched
|
6 months
annual
high
successful
daytime
ground-based
|
|
gptkbp:launchSite
|
gptkb:Semnan_Space_Center
500 kg
trained personnel
|
|
gptkbp:launchVehicle
|
Kavoshgar
Kavoshgar_series
|
|
gptkbp:manufacturer
|
Iran_Space_Agency
|
|
gptkbp:maximumDepth
|
100 km
|
|
gptkbp:mediaCoverage
|
extensive
|
|
gptkbp:mission
|
suborbital
|
|
gptkbp:missions
|
short-term
|
|
gptkbp:nationality
|
Iranian
|
|
gptkbp:operationalStatus
|
2010
low
|
|
gptkbp:passenger_traffic
|
biological samples
|
|
gptkbp:payloadCapacity
|
100 kg
|
|
gptkbp:productionCompany
|
operational
|
|
gptkbp:propulsion
|
20 kN
|
|
gptkbp:provides
|
inertial navigation
|
|
gptkbp:publicAccess
|
high
|
|
gptkbp:purpose
|
scientific research
|
|
gptkbp:relatedPatent
|
gptkb:Simorgh_rocket
|
|
gptkbp:renovated
|
parachute
|
|
gptkbp:researchInterest
|
Iranian_universities
|
|
gptkbp:safetyFeatures
|
redundant systems
|
|
gptkbp:scientificName
|
microgravity experiments
|
|
gptkbp:succeededBy
|
true
|
|
gptkbp:technology
|
available
|
|
gptkbp:weight
|
500 kg
|