RD-0120
The Soviet RD-0120 (also designated 11D122) was the Energia core rocket engine, fueled by LH2/LOX, roughly equivalent to the Space Shuttle Main Engine (SSME). These were attached to the Energia core rather than the orbiter, so were not recoverable after a flight, but created a more modular design (the Energia core could be used for a variety of missions besides launching the shuttle). Baselined from the more mature American hydrogen–oxygen engine technology, but considerably modified with Russian innovations and methods, the RD-0120 and the SSME have both similarities and differences. The RD-0120 achieved nearly identical specific impulse and combustion chamber pressure with reduced complexity and cost, as compared to the SSME, primarily at the expense of lower thrust-to-weight ratio. It u
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RD-0120
The Soviet RD-0120 (also designated 11D122) was the Energia core rocket engine, fueled by LH2/LOX, roughly equivalent to the Space Shuttle Main Engine (SSME). These were attached to the Energia core rather than the orbiter, so were not recoverable after a flight, but created a more modular design (the Energia core could be used for a variety of missions besides launching the shuttle). Baselined from the more mature American hydrogen–oxygen engine technology, but considerably modified with Russian innovations and methods, the RD-0120 and the SSME have both similarities and differences. The RD-0120 achieved nearly identical specific impulse and combustion chamber pressure with reduced complexity and cost, as compared to the SSME, primarily at the expense of lower thrust-to-weight ratio. It u
has abstract
Das RD-0120 (von russisch Реак ...... ich geringeren Schub erreicht.
@de
El RD-0120 (también designado ...... acústica que el SSME requería.
@es
Le RD-0120 est un moteur-fusée ...... programme de la fusée Energia.
@fr
RD-0120 (11D122としても認識される)はスペース ...... Eでは必要な音響共鳴燃焼室を使用せずに燃焼の安定を達成する。
@ja
RD-0120 是苏联能源号运载火箭的芯级发动机。相当于美国 ...... 装置。每 台发动机的真空推力200 t,真空比冲455 s。
@zh
RD-0120: silnik rakietowy prod ...... instalować go wewnątrz promu.
@pl
The Soviet RD-0120 (also desig ...... ambers that the SSME required.
@en
РД-0120 — жидкостный ракетный ...... лено четыре двигателя РД-0120.
@ru
Link from a Wikipage to an external page
Wikipage page ID
15,698,501
Wikipage revision ID
741,589,195
associated
burn time
Caption
Model of RD-0120
combustion chamber
country of Origin
designer
first date
1987-05-15
fuel
image size
last date
1988-11-15
manufacturer
mixture ratio
nozzle ratio
oxidiser
purpose
Sustainer engine
successor
thrust to weight
used in
Energia core stage
subject
hypernym
type
comment
Das RD-0120 (von russisch Реак ...... ich geringeren Schub erreicht.
@de
El RD-0120 (también designado ...... mplejidad y coste reducidos, p
@es
Le RD-0120 est un moteur-fusée ...... euls vols d'Energia en 1987 et
@fr
RD-0120 (11D122としても認識される)はスペース ...... Eでは必要な音響共鳴燃焼室を使用せずに燃焼の安定を達成する。
@ja
RD-0120 是苏联能源号运载火箭的芯级发动机。相当于美国 ...... 装置。每 台发动机的真空推力200 t,真空比冲455 s。
@zh
RD-0120: silnik rakietowy prod ...... instalować go wewnątrz promu.
@pl
The Soviet RD-0120 (also desig ...... r thrust-to-weight ratio. It u
@en
РД-0120 — жидкостный ракетный ...... лено четыре двигателя РД-0120.
@ru
label
RD-0120
@de
RD-0120
@en
RD-0120
@es
RD-0120
@fr
RD-0120
@ja
RD-0120
@pl
RD-0120
@zh
РД-0120
@ru