- The
staged combustion cycle (sometimes
known as
topping cycle,
preburner cycle, or
closed cycle) is a
power cycle of a
bipropellant rocket engine. In...
- only hydrogen,
allowing for
greater specific impulse. The RD-701 has two
preburners per
combustion chamber, both of
which run
oxygen rich. One is used to...
- twin-shaft
staged combustion cycle that uses both oxidizer-rich and fuel-rich
preburners. The
cycle allows for the full flow of both
propellants through the turbines...
-
employs an oxygen-rich
preburner,
unlike typical fuel-rich US designs. The
thermodynamics of the
cycle allow an oxygen-rich
preburner to give a
greater power-to-weight...
-
caused an RSLS
shutdown at T−3
seconds due to a leak in its liquid-oxygen
preburner check valve. STS-51
Discovery – No. 2
engine caused an RSLS shut down...
- full-duration burns, and one that
supports short-duration, high-pressure
preburner tests. The
spaceport also
includes a
vehicle processing facility and an...
-
bipropellant liquid rocket engines.
Propellant is
burned in a gas
generator (or "
preburner") and the
resulting hot gas is used to
power the
propellant pumps before...
-
Shuttle uses a
system of
fluted posts,
which use
heated hydrogen from the
preburner to
vaporize the
liquid oxygen flowing through the
center of the posts...
- air/hydrogen
injectors for the
SABRE preburners. In 2020,
Airborne Engineering conducted a test
campaign on an "HX3 module" (
preburner to
helium loop heat exchanger)...
- main
combustion chamber exhaust rather than a
separate gas
generator or
preburner. The J-2S
rocket engine, a
cancelled engine developed by NASA, used the...
