RD-861
The RD-861 is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle. It has a main combustion chamber, with four vernier nozzles fed by the gas generator output. It can be reignited a single time.
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RD-861
The RD-861 is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle. It has a main combustion chamber, with four vernier nozzles fed by the gas generator output. It can be reignited a single time.
has abstract
The RD-861 is a Soviet liquid ...... an be reignited a single time.
@en
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Wikipage page ID
51,009,788
Wikipage revision ID
741,589,649
associated
Tsyklon-2 and Tsyklon-3
burn time
combustion chamber
country of Origin
designer
first date
1967-10-27
fuel
manufacturer
mixture ratio
nozzle ratio
oxidiser
predecessor
purpose
specific impulse vacuum
status
Out of production
successor
used in
Tsyklon-2 and Tsyklon-3 third stage
subject
comment
The RD-861 is a Soviet liquid ...... an be reignited a single time.
@en
label
RD-861
@en