-
Vinci is a
restartable, cryogenic, liquid-propellant
rocket engine that
powers the
upper stage of
Ariane 6.
While development began in 1998 for the planned...
- The
Reaction Motors LR99
engine was the
first large, throttleable,
restartable liquid-propellant
rocket engine.
Development began in the 1950s by the...
-
restarting the
component that is affected. This
entails both
modularity and
restartability.
Components should be
restarted before they fail, and
designed to make...
-
which a
General Electric GEnx-1B PIP2
engine suffered damage and non-
restartable power loss
while flying at an
altitude of 20,000 feet. The
damage is...
-
dramatically improved performance compared to
older protocols,
ZMODEM offered restartable transfers, auto-start by the sender, an
expanded 32-bit CRC, and control...
- reused.
There are two
versions of the
upper stage, one
hypergolic and
restartable with a
single Aestus engine and the
other with a HM7B
cryogenic engine...
- fuel with LOX, to
produce 200,000 pounds-force (890 kN) of thrust. A
restartable version of the S-IVB was used as the
third stage of the
Saturn V. The...
-
residual liquid hydrogen fuel. This
mission supported the
design of the
restartable version of the S-IVB used in the
Saturn V, by
observing the behavior...
- on the Moon. For the
Apollo lunar missions, TLI was
performed by the
restartable J-2
engine in the S-IVB
third stage of the
Saturn V rocket. This particular...
-
developed for the
Apollo program. By the '90s,
development on
large reliable restartable rocket engines made it
possible to use the
already matured technology...
