RD-107 A-1

URI: https://gptkb.org/entity/RD-107_A-1
GPTKB entity
Statements (61)
Predicate Object
gptkbp:instance_of gptkb:rocket
gptkbp:bfsLayer 5
gptkbp:bfsParent gptkb:RD-107_A_engine
gptkbp:aircraft_operated gptkb:Soyuz
gptkb:Vostok
gptkbp:application space launch vehicles
gptkbp:controls gptkb:military_officer
variable
gptkbp:cooling_system regenerative cooling
gptkbp:designed_by OKB-456
gptkbp:developer 1950s
gptkbp:diameter 1.5 m
gptkbp:emissions_standard bell nozzle
gptkbp:engine gptkb:OKB-1
1970s
mass production
open cycle
hypergolic
single chamber
influenced modern rocket engines
gimbal mount
gptkbp:engine_type staged combustion
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
RD-107 A-11
RD-107 A-12
RD-107 A-13
RD-107 A-14
RD-107 A-15
RD-107 A-16
RD-107 A-17
RD-107 A-18
RD-107 A-19
RD-107 A-20
gptkbp:first_flight gptkb:1957
gptkbp:fuel_capacity 2.5 kg/s
gptkbp:fuel_type 3200 K
gas-generator cycle
kerosene
https://www.w3.org/2000/01/rdf-schema#label RD-107 A-1
gptkbp:ignition_system gptkb:park
gptkbp:is_tested_for static fire test
gptkbp:length 3.5 m
gptkbp:metabolism 3.5 kg/s
gptkbp:number_of_rooms 6.5 M Pa
gptkbp:origin gptkb:Monarch
gptkbp:propulsion 300 s
1000 k N
gptkbp:social_structure liquid oxygen
gptkbp:status retired
gptkbp:successor gptkb:RD-108
gptkbp:type gptkb:rocket
gptkbp:used_in gptkb:R-7_Semyorka
gptkbp:weight 800 kg