About: Agnibaan

Property	Value
dbo:MeanOfTransportation/diameter	1.3 (dbd:metre)
dbo:MeanOfTransportation/height	18000.0 (dbd:millimetre)
dbo:MeanOfTransportation/mass	14000.0 (dbd:kilogram)
dbo:Rocket/lowerEarthOrbitPayload	100.0 (dbd:kilogram)
dbo:Rocket/mass	14000.0 (dbd:kilogram)
dbo:abstract	Agnibaan (Agni - Fire, Baan - Arrow, lit. Arrow of fire), produced by Agnikul Cosmos in Chennai, India, is a mobile launch system currently under development. It is capable of placing a 100 kg (220 lb) satellite into a 700 km (430 mi) orbit. The rocket will be 18 meters long with a diameter of 1.3 meters and a lift-off mass of 14,000 kg (31,000 lb). The rocket is supposed to be manufactured by 3D printing as a whole. The Agnibaan rocket has three stages. The first stage is powered by seven Agnite engines. The second stage is powered by the same Agnite engine which will have a larger nozzle than the sea level nozzle to optimize it for vacuum. (en)
dbo:diameter	1.300000 (xsd:double)
dbo:height	18.000000 (xsd:double)
dbo:lowerEarthOrbitPayload	100000.000000 (xsd:double)
dbo:manufacturer	dbr:Agnikul_Cosmos
dbo:mass	14000000.000000 (xsd:double)
dbo:rocketFunction	dbr:Launch_Vehicle
dbo:rocketStages	3 (xsd:nonNegativeInteger)
dbo:status	Under Development
dbo:wikiPageID	69858255 (xsd:integer)
dbo:wikiPageLength	5505 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	1120022875 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Electric-pump-fed_engine dbr:Department_of_Space dbr:Vikram_1 dbr:List_of_orbital_launch_systems dbr:Skyroot_Aerospace dbr:Kerosene dbc:Space_launch_vehicles_of_India dbc:Vehicles_introduced_in_2022 dbr:Liquid_oxygen dbr:AgniKul_Cosmos dbr:3D_printing dbc:Spacecraft dbr:Agnikul_Cosmos dbr:Indian_Space_Research_Organisation dbr:RP-1 dbr:Launch_Vehicle dbr:LOX dbr:Small-lift_launch_vehicle dbr:Chennai,_India dbr:Alaska_Aerospace_Corporation
dbp:countryOrigin	India (en)
dbp:diameter	1.3 m (en)
dbp:first	NET 2022 (en)
dbp:function	dbr:Launch_Vehicle
dbp:height	18 m (en)
dbp:leoPayload	Altitude 700 km Orbital inclination 45.0° Mass 100 kg (en)
dbp:manufacturer	dbr:Agnikul_Cosmos
dbp:mass	14000.0 (dbd:kilogram)
dbp:name	Agnibaan Launch Vehicle (en)
dbp:stage1engines	7 (xsd:integer)
dbp:stage1fuel	dbr:RP-1 dbr:LOX
dbp:stage1thrust	140 kN (en)
dbp:stage1time	285.0 (dbd:second)
dbp:stage2engines	Agnite (en)
dbp:stage2fuel	dbr:RP-1 dbr:LOX
dbp:stage2thrust	25 kN (en)
dbp:stage2time	355.0 (dbd:second)
dbp:stage3engines	Agnilet (en)
dbp:stage3fuel	dbr:RP-1 dbr:LOX
dbp:stages	3 (xsd:integer)
dbp:status	Under Development (en)
dbp:wikiPageUsesTemplate	dbt:Reflist dbt:Infobox_rocket
dct:subject	dbc:Space_launch_vehicles_of_India dbc:Vehicles_introduced_in_2022 dbc:Spacecraft
rdf:type	owl:Thing dbo:MeanOfTransportation wikidata:Q41291 dbo:Rocket
rdfs:comment	Agnibaan (Agni - Fire, Baan - Arrow, lit. Arrow of fire), produced by Agnikul Cosmos in Chennai, India, is a mobile launch system currently under development. It is capable of placing a 100 kg (220 lb) satellite into a 700 km (430 mi) orbit. The rocket will be 18 meters long with a diameter of 1.3 meters and a lift-off mass of 14,000 kg (31,000 lb). The rocket is supposed to be manufactured by 3D printing as a whole. The Agnibaan rocket has three stages. The first stage is powered by seven Agnite engines. The second stage is powered by the same Agnite engine which will have a larger nozzle than the sea level nozzle to optimize it for vacuum. (en)
rdfs:label	Agnibaan (en)
owl:sameAs	wikidata:Agnibaan dbpedia-hu:Agnibaan https://global.dbpedia.org/id/GHRF7
prov:wasDerivedFrom	wikipedia-en:Agnibaan?oldid=1120022875&ns=0
foaf:isPrimaryTopicOf	wikipedia-en:Agnibaan
foaf:name	Agnibaan Launch Vehicle (en)
is dbo:wikiPageWikiLink of	dbr:List_of_private_spaceflight_companies dbr:List_of_orbital_launch_systems dbr:Comparison_of_orbital_launch_systems dbr:Skyroot_Aerospace dbr:Byomkesh_Bakshi_in_other_media dbr:2022_in_spaceflight dbr:AgniKul_Cosmos dbr:Pacific_Spaceport_Complex_–_Alaska dbr:Small-lift_launch_vehicle
is foaf:primaryTopic of	wikipedia-en:Agnibaan