Pat
1. The choice of hydrogen peroxide and JP-8 as propellants may be
telling
> in this regard also;
2. It would also explain with they haven't released photos of the
underside
> of the X-37B, as those would show the attachment points to the ET, as
> well as where the the JP-8 and H2O2 plumbing from the ET goes into the
> orbiter.
1. The propellants were changed to N2O4 and MMH
2. The engines don't have the thrust
It was never intended for this. It is a spacecraft that can return
from space and not a launch vehicle. It was already designed and
built when NASA managed the program.
That needs adding to the Wikipedia article then, as it doesn't mention
it, although some other websites do.
That would also avoid the frost problem, and probably give better isp to
boot.
> 2. The engines don't have the thrust
In the early Boeing concept shown in the PM cover, the engines (RL10s)
were to run off of LOX/LH2, which made for a large ET due to the low
density of the LH2.
As I pointed out, to do this launch concept you would have to add more
engines to it, although the X-37B could serve as a aerodynamic test
vehicle for such a derivative.
> It was never intended for this. It is a spacecraft that can return
> from space and not a launch vehicle. It was already designed and
> built when NASA managed the program.
Well, the Air Force has it now, and if it takes a Atlas V to boost it
into orbit, its whole purpose seems baffling.
http://www.foxnews.com/story/0,2933,569143,00.html
(That gets us back to the Boeing artwork of one with RVs riding on the
wings:http://www.msnbc.msn.com/id/3077821/
But sooner or later the thing has to land, and what's it supposed to do
with the RVs then?)
It's supposed to check out advanced technologies, but those technologies
are supposed to be used on what exactly?
Back when it was part of the Future-X program, that program also
included reusable launch vehicle studies:
http://www.designation-systems.net/dusrm/app4/x-37.html
Pat
> Well, the Air Force has it now, and if it takes a Atlas V to boost it
> into orbit, its whole purpose seems baffling.
If not Atlas V, or Delta IV (?) then what is there for a U.S. military
lift? Is it as "reliable" as Atlas V? Perhaps Atlas V is overkill,
but if you don't have funding for too many tries, perhaps the more
reliable, but more costly overspec'ed, launcher is apropriate at this
stage?
rick jones
--
I don't interest myself in "why". I think more often in terms of
"when", sometimes "where"; always "how much." - Joubert
these opinions are mine, all mine; HP might not want them anyway... :)
feel free to post, OR email to rick.jones2 in hp.com but NOT BOTH...