RD-0110 engine

URI: https://gptkb.org/entity/RD-0110_engine

GPTKB entity

Statements (68)

Predicate	Object
gptkbp:instance_of	gptkb:Team_Rocket
gptkbp:aircraft_operated	gptkb:Soyuz-U gptkb:Soyuz-FG gptkb:Soyuz-2.1b gptkb:Soyuz-2.1c gptkb:Soyuz-2.1d gptkb:Soyuz-2.1e gptkb:Soyuz-2.1f gptkb:Soyuz-2.1g gptkb:Soyuz-2.1h gptkb:Soyuz-2.1i gptkb:Soyuz-2.1j gptkb:Soyuz-2.1k gptkb:Soyuz-2.1m gptkb:Soyuz-2.1n gptkb:Soyuz-2.1o gptkb:Soyuz-2.1p gptkb:Soyuz-2.1q gptkb:Soyuz-2.1r gptkb:Soyuz-2.1s gptkb:Soyuz-2 gptkb:Soyuz-2.1v gptkb:Soyuz-2.1a gptkb:Soyuz-STA gptkb:Soyuz-2.1l gptkb:Soyuz-2.1t gptkb:Soyuz-2.1u gptkb:Soyuz-2.1w gptkb:Soyuz-2.1x gptkb:Soyuz-2.1y gptkb:Soyuz-2.1z
gptkbp:application	launch vehicles
gptkbp:check_in_time	150 seconds
gptkbp:combustor_type	3000 K staged combustion
gptkbp:debut	gptkb:1965
gptkbp:designed_by	gptkb:Kuznetsov_Design_Bureau
gptkbp:development	gptkb:Soviet_Union 1960s
gptkbp:engine	gptkb:RD-0124 staged combustion cycle RD-0115
gptkbp:engine_configuration	vertical
gptkbp:exhaust_system	bell nozzle
gptkbp:first_flight	gptkb:1966
gptkbp:fuel_capacity	1.5 m 3.5 m
gptkbp:fuel_type	gptkb:RP-1 kerosene
https://www.w3.org/2000/01/rdf-schema#label	RD-0110 engine
gptkbp:inspiration	RD-0105
gptkbp:manufacturer	gptkb:Kuznetsov
gptkbp:number_of_rooms	two 20 MPa
gptkbp:operational_use	crew and cargo missions
gptkbp:oxidation_states	gptkb:LOX liquid oxygen
gptkbp:propulsion	250 100 k N
gptkbp:specific_impulse	300 seconds
gptkbp:status	in service
gptkbp:successor	gptkb:RD-0120
gptkbp:type	liquid-fueled
gptkbp:used_in	gptkb:Soyuz_spacecraft
gptkbp:weight	400 kg
gptkbp:bfsParent	gptkb:spacecraft gptkb:Soyuz_spacecraft
gptkbp:bfsLayer	4