Hot Fire: XCOR Aerospace and United Launch Alliance
Achieve Major Milestone in Liquid Hydrogen Engine
Program
Nov. 19, 2013
XCOR Aerospace and United
Launch Alliance (ULA) announced a significant
milestone today, the first successful hot fire of
the subscale 2500 lbf thrust XR-5H25 engine in the
XCOR® and ULA liquid hydrogen (LH2)
engine development program.
"The first hot fire of any
engine is a major milestone but the first firing of
a liquid hydrogen engine in our LH2 program is an
even bigger accomplishment," noted XCOR Chief
Executive Officer
Jeff Greason.
"The hot fire of this engine moves us forward on a
path to routine tests and further demonstration of
fully reusable, high reliability rocket engines for
which we are known."
"XCOR's ability to develop
inexpensive, innovative and out-of-the-box solutions
to some of the most challenging problems in modern
cryogenic rocket engine technology was on display in
Mojave," said
George Sowers,
vice president of Strategic Architecture at ULA. "It
was a great first set of engine runs and we look
forward to seeing the engine and XCOR's unique
piston pumps integrated together in 2014."
Conceived as a lower-cost,
risk-managed approach, the goal of the XCOR/ULA LH2
engine program is to produce and operate a subscale
demonstration engine. This demonstrator will
enable a future decision to pursue development of a
flight-ready cryogenic upper-stage engine in the
25,000 lbf thrust class. The technology has
significant growth potential due to its unique
thermodynamic cycle and piston pump. The larger
thrust XCOR XR-8H21 LH2 engine should cost
significantly less to produce and be much easier to
operate than competing upper stage rocket engine
technologies.
XCOR Chief Operating
Officer
Andrew Nelson
said, "I was very impressed with how our team
dedicated itself to achieving a task that has not
been accomplished in at least a quarter century,
maybe more; the development of a new way to do
liquid hydrogen rocket engines that fundamentally
breaks current cost, reliability and operational
models. Even more than that, it will be the first
piston-pump-fed LH2 rocket engine anywhere."
The 5H25 engine is
intended as a testbed, but could also be suitable
for future in-space use on upper stages, earth
departure stages, landers, and probes. Nelson added,
"This is a significant leap forward in the hope to
deliver yet another line of innovation and business
to XCOR. And it is only taking place right here."