RD-107 A engine

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:rocket
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:Soyuz_MS-19
gptkbp:application space launch vehicles
gptkbp:check_in_time 150 s
gptkbp:cooling_system regenerative cooling
gptkbp:designed_by OKB-456
gptkbp:developer 1955-1957
gptkbp:diameter 1.5 m
gptkbp:engine gptkb:RD-108
gptkb:Monarch
gptkb:RD-0120
post-World War II
staged combustion
high thrust-to-weight ratio
RD-0110
crew and cargo missions
liquid propulsion
influenced future rocket designs
detailed technical data
multi-chamber
RD series
four-chamber
gptkbp:engine_type gptkb:RD-107_A-1
staged combustion engine
RD-107 A-10
RD-107 A-2
RD-107 A-3
RD-107 A-4
RD-107 A-5
RD-107 A-6
RD-107 A-7
RD-107 A-8
RD-107 A-9
gptkbp:first_flight gptkb:1957
gptkbp:fuel_type gas-generator cycle
kerosene
https://www.w3.org/2000/01/rdf-schema#label RD-107 A engine
gptkbp:inspiration gptkb:V-2_rocket_engine
gptkbp:is_tested_for static fire tests
gptkbp:length 3.5 m
gptkbp:notable_album gptkb:Sputnik_1
gptkbp:number_of_rooms gptkb:4
6.5 M Pa
gptkbp:operational_area gptkb:Soviet_space_program
gptkbp:propulsion 300 s
100 k N
gptkbp:social_structure liquid oxygen
gptkbp:status retired
gptkbp:successor gptkb:RD-108_engine
gptkbp:type liquid-fueled engine
gptkbp:used_in gptkb:R-7_Semyorka
gptkbp:weight 1,200 kg