posted on Sep, 2 2004 @ 06:52 PM
www.aerospaceweb.org...
Why is hydrogen used as fuel in a scramjet engine?
- name withheld
In order to better understand this question, we must first understand some of the fundamental hurdles that must be overcome in operating a supersonic
combustion ramjet (scramjet). Scramjets are designed to operate in the hypersonic regime of flight. A vehicle using such an engine typically flies
faster than Mach 5, or 5 times the speed of sound since this speed is generally accepted as the beginning of the hypersonic regime. Flight at such
speeds is nothing new. After all, Air Force test pilot and current California state senator Pete Knight set an unofficial world speed record on 3
October 1967 when he flew the X-15 research plane upwards of Mach 6.7. At its peak altitude of over 350,000 ft (107,900 m), that speed corresponds to
about 4,530 mph (7,300 km/h).
You really should know what you are talking about first before you post saying something I have posted is "un true"
www.aviation-history.com...
Scramjet is an acronym for Supersonic Combustion Ramjet. The scramjet differs from the ramjet in that combustion takes place at supersonic air
velocities through the engine. It is mechanically simple, but vastly more complex aerodynamically than a jet engine. Hydrogen is normally the fuel
used.
"air" in the normal sense of the word as people typically imply "oxygen" is not really what is happening in a Scramjet. Its really the
"friction" of the particles moving at high-supersonic speed over the combustor section that is the medium when mixed with hydrogen to sustain the
thrust in a scramjet engine. The actual makeup of the inlet componet really does not matter as long as it includes HYDROGEN driven at high velocity,
in fact if you could run the scramject in only a hydrogen rich atmoshpere you could limit the amount of "fuel" you would have to use to sustain
hypersonic flight.
Provided of course you first got the "thing" up to hypersonic speed to begin with, by solid rocket or whatever means needed.
www.tfd.chalmers.se...
This is the detailed report from los Alamos Labs/ Sandia Labs about Hypersonic Hydrogen combustion. The only critical component is Hydrogen when they
state the compressed "air" they actual use a H2 and C2H4 mixture that mimick the density of atmospheric "air" knowing that Oxygen or "air" is
not required to sustain hypersonic combustion. Its actually the compression and density of the input "air" to the required heating and then the
interjection of the Hydrogen fuel that causes autoignition. There is no mention about the need for a specific oxidizor, noting that Hydrogen subjected
to hypersonic compression will autoignite
[edit on 2-9-2004 by robertfenix]
[edit on 2-9-2004 by robertfenix]
[edit on 2-9-2004 by robertfenix]