RD-0110R
The RD-0110R (GRAU Index 14D24) is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four nozzles that can gimbal up to 45 degrees in a single axis and is used as the vernier thruster on the Soyuz-2-1v first stage. It also has heat exchangers that heats oxygen and He to pressurize the LOX and RG-1 tanks of the Soyuz-2.1v first stage, respectively. The Oxygen is supplied from the same LOX tank in liquid form, while the He is supplied from separate high pressure bottles (known as the T tank).
primaryTopic
RD-0110R
The RD-0110R (GRAU Index 14D24) is a rocket engine burning liquid oxygen and kerosene in a gas generator combustion cycle. It has four nozzles that can gimbal up to 45 degrees in a single axis and is used as the vernier thruster on the Soyuz-2-1v first stage. It also has heat exchangers that heats oxygen and He to pressurize the LOX and RG-1 tanks of the Soyuz-2.1v first stage, respectively. The Oxygen is supplied from the same LOX tank in liquid form, while the He is supplied from separate high pressure bottles (known as the T tank).
has abstract
The RD-0110R (GRAU Index 14D24 ...... the Voronezh Mechanical Plant.
@en
РД-0110Р (14Д24) — жидкостный ...... ронежском механическом заводе.
@ru
Link from a Wikipage to an external page
Wikipage page ID
46,864,355
Wikipage revision ID
741,589,481
associated
burn time
combustion chamber
country of Origin
designer
KBKhA, Viktor Gorokhov
first date
2013-12-28
manufacturer
oxidiser
predecessor
specific impulse sea level
specific impulse vacuum
status
used in
Soyuz-2-1v first stage.
subject
hypernym
comment
The RD-0110R (GRAU Index 14D24 ...... bottles (known as the T tank).
@en
РД-0110Р (14Д24) — жидкостный ...... ронежском механическом заводе.
@ru
label
RD-0110R
@en
РД-0110Р
@ru