RD-0110
The RD-0110 is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four fixed nozzles and the output of the gas generator is directed to four secondary vernier nozzles to supply vector control of the stage. It has an extensive flight history with its initial versions having flown more than 55 years ago (as of June 2015).
RD-0110
The RD-0110 is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four fixed nozzles and the output of the gas generator is directed to four secondary vernier nozzles to supply vector control of the stage. It has an extensive flight history with its initial versions having flown more than 55 years ago (as of June 2015).
has abstract
Le RD-0110 est un moteur-fusée ...... s russes de la famille Soyouz.
@fr
RD-0110は液体酸素とケロシンを推進剤として使用するガス ...... vで使用されるブロックIでは後継のRD-0124を搭載する。
@ja
The RD-0110 is a rocket engine ...... 5 years ago (as of June 2015).
@en
РД-0110 (11Д55 по классификаци ...... «Союз» и «Молния-М» (Блок И).
@ru
thumbnail
Link from a Wikipage to an external page
Wikipage page ID
46,839,897
Wikipage revision ID
742,535,300
associated
Molniya-M and Soyuz
burn time
combustion chamber
country of Origin
designer
first date
1965-10-05
manufacturer
mixture ratio
oxidiser
predecessor
purpose
specific impulse vacuum
status
thrust to weight
used in
Molniya-M Block-I and on most Soyuz Block-I
subject
hypernym
comment
Le RD-0110 est un moteur-fusée ...... s russes de la famille Soyouz.
@fr
RD-0110は液体酸素とケロシンを推進剤として使用するガス ...... vで使用されるブロックIでは後継のRD-0124を搭載する。
@ja
The RD-0110 is a rocket engine ...... 5 years ago (as of June 2015).
@en
РД-0110 (11Д55 по классификаци ...... «Союз» и «Молния-М» (Блок И).
@ru
label
RD-0110
@en
RD-0110
@fr
RD-0110
@ja
РД-0110
@ru
