A Space & astronomy forum. SpaceBanter.com

Go Back   Home » SpaceBanter.com forum » Space Science » Policy
Site Map Home Authors List Search Today's Posts Mark Forums Read Web Partners

Ares vs Delta or Atlas



 
 
Thread Tools Display Modes
  #1  
Old January 26th 09, 10:48 AM posted to sci.space.policy
Fred J. McCall[_3_]
external usenet poster
 
Posts: 10,018
Default Ares vs Delta or Atlas

Pat Flannery wrote:
:
:Fred J. McCall wrote:
: :If you did make a rocket engine that, say, used two separate turbopumps
: :to drive its four combustion chambers... yeah, I'd agree to that being
: :two separate rocket engines despite what the designers called it or how
: :the wiring or plumbing on it worked.
: :
:
: Why? Just based on the number of pumps? We just saw that break down
: for your automotive example. Is it any better definition here?
:
:
:It didn't break down for my automotive example.
:

It certainly did initially, where you started out saying that if there
was a single fuel pump then it was a single engine (like your 'single
turbopump' argument for rocket engines). Then I pointed out that a
fuel injected engine with multiple fuel pumps would not necessarily be
too odd, at which point you switched to 'more than one engine block'.

:
:If the Cadillac V-16 engine consisted of two separate Cadillac V-8
:engines connected to a single transmission system, I would have no
roblem at all calling it a two-engine system.
:But it used a single carburetor and electrical system connected to all
:16 cylinders mounted in a single engine block.
:Even if it had consisted of two separate V-8 engine blocks connected to
:a single drive shaft front-to-back but using a single electrical system,
:distributer to fire the spark plugs appropriately, and carburetor to
:feed all sixteen cylinders the correct fuel-air mixture - as well as the
:timing gears that opened and closed all sixteen intake and exhaust
:valves at the appropriate times to make the engine work properly, then
:it's a single engine.
:Split the two engine blocks apart, and at least one of them will be
:nonfunctional, as it no longer has a carburetor system to send fuel and
:air to its cylinders, will have its timing way off due to the missing
:eight cylinders, and won't posses a distributer to fire its spark plugs.
:

So how do you decide where 'the engine' stops?

: : : If I ta
:
: You talked a lot, but the answer is weak. Now lets take a progression
: and see how many engines we're talking about at each stage by your
: definitions:
:
: Start with a pressurized system with four chambers and four nozzles.
: Since there is no pump, presumably this is counted as four engines,
: just like the example of the solids.
:
:But again , you're talking hypothetical rocket systems - not anything
:anyone has really built due to their obvious shortcomings.
:

Of course I am. Any good taxonomy will cover everything, not just
stuff you've currently seen.

:
:You can make a good case for the original pressure-fed version of the
:four barreled XLR-11 used in the original X-1 flights as being a single
r multiple rocket engine... but what's your point? It only existed in
:the four-barreled version, and no one ever suggested making a
:two-barreled or six-barreled version of it.
:When it did get a turbopump in the later version it was a single
:turbopump feeding all four combustion chambers, and it was still
:described as a XLR-11 with the turbopump simply replacing the pressure
:feed system.
:

So to your mind it suddenly (perhaps) transmogrifies from multiple
engines when pressure fed to being a single engine when fed by
turbopump. So IDENTICALLY THE SAME HARDWARE changes from a multiple
engines to a single engine or back depending solely on what is used to
pressurize the propellants?

That just doesn't seem to make sense, Pat.

:
:
: Now add a single set of turbopumps with no other changes. Now,
: according to you, the original four engines are magically transformed
: into one engine.
:
:
:That would be exactly the case, as none of the engine's individual
:combustion chambers can work on its own without that turbopump feeding
:it fuel and oxidizer.
:

Again, multiple engines suddenly transmogrify into a single engine
based solely on how the propellant is pressurized.

Again, that just doesn't seem to make sense.

: Now add three more sets of turbopumps. It's suddenly four engines
: again.
:
: What happens if instead of adding a pump for propellant and oxidizer,
: we only add propellant pumps and leave the oxidizer pressure-fed? Now
: what is it?
:
:
:Again, what you are doing is creating philosophical concepts, not real
:hardware that has ever been built - to try to create some sort of
:razor's edge description of what a thing is via sophistry.
:

No, I'm just trying to point out where your taxonomic system breaks
down. And it *does* break down.


--
"Some people get lost in thought because it's such unfamiliar
territory."
--G. Behn
 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
Comparison of Delta IV, Aries 1 and Atlas V M History 25 December 21st 08 08:23 PM
Once mo Man Rating Delta IV and Atlas V [email protected] Policy 5 March 3rd 05 04:24 AM
Atlas - Delta Very Heavy William J Hubeny Space Science Misc 17 May 8th 04 01:03 AM
Delta IV vs. Atlas V ed kyle Policy 51 August 24th 03 03:43 AM
7 Delta-IV launches will be transfered to Atlas-V Gunter Krebs Policy 2 July 27th 03 12:01 PM


All times are GMT +1. The time now is 05:38 AM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 SpaceBanter.com.
The comments are property of their posters.