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Stick Second Stage and Delta IV



 
 
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  #1  
Old September 7th 05, 10:44 PM
Ed Kyle
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Default Stick Second Stage and Delta IV

Has anyone else noticed that the proposed
SRB/SSME "Stick" vehicle has a second stage
diameter that is roughly the same as the
diameter of the Delta IV Common Booster
Core (5.1 meters)? And, by the way, that
the SRB/SSME second stage length seems to
be not much less than the length of a CBC?

- Ed Kyle

  #2  
Old September 7th 05, 11:01 PM
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Has anyone else noticed that the proposed SRB/SSME "Stick" vehicle has a second stage diameter that is roughly the same as the diameter of the Delta IV Common Booster Core (5.1 meters)?

Yep. Including ATK.

  #3  
Old September 7th 05, 11:12 PM
Alex Terrell
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Ed Kyle wrote:
Has anyone else noticed that the proposed
SRB/SSME "Stick" vehicle has a second stage
diameter that is roughly the same as the
diameter of the Delta IV Common Booster
Core (5.1 meters)? And, by the way, that
the SRB/SSME second stage length seems to
be not much less than the length of a CBC?

Coincidence or Cooperation?

I guess the White Elephant second stage diameter is driven by the CEV
diameter and the length is then driven by the propellant required.

Using a Delta IV common booster would save a lot of development work,
but that rather defeats the puropose of the Stick.

  #4  
Old September 8th 05, 12:29 AM
Scott Lowther
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Alex Terrell wrote:

Ed Kyle wrote:


Has anyone else noticed that the proposed
SRB/SSME "Stick" vehicle has a second stage
diameter that is roughly the same as the
diameter of the Delta IV Common Booster
Core (5.1 meters)? And, by the way, that
the SRB/SSME second stage length seems to
be not much less than the length of a CBC?



Coincidence or Cooperation?

I guess the White Elephant second stage diameter is driven by the CEV
diameter and the length is then driven by the propellant required.

Using a Delta IV common booster would save a lot of development work,
but that rather defeats the puropose of the Stick.



Not really. Practically, just about all that would be used on a
Stick/DIV vehicle from the DIV woud be the tanks, payload interface and
some of the plumbing, and even the tanks would be changed (shortened).
Development would still be required, but at least the tooling would be
in place for some of the major hardware.

--
"The only thing that galls me about someone burning the American flag is how unoriginal it is. I mean if you're going to pull the Freedom-of-speech card, don't be a hack, come up with something interesting. Fashion Old Glory into a wisecracking puppet and blister the system with a scathing ventriloquism act, or better yet, drape the flag over your head and desecrate it with a large caliber bullet hole." Dennis Miller
  #5  
Old September 8th 05, 01:27 AM
Ed Kyle
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Default

Scott Lowther wrote:

.. Practically, just about all that would be used on a
Stick/DIV vehicle from the DIV woud be the tanks, payload interface and
some of the plumbing, and even the tanks would be changed (shortened).
Development would still be required, but at least the tooling would be
in place for some of the major hardware.


Hmmmmmm.

"Stick/DIV".

S-DIV.

S-IVD?

- Ed Kyle

  #6  
Old September 8th 05, 01:50 AM
Brian Thorn
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Default

On 7 Sep 2005 17:27:25 -0700, "Ed Kyle" wrote:

.. Practically, just about all that would be used on a
Stick/DIV vehicle from the DIV woud be the tanks, payload interface and
some of the plumbing, and even the tanks would be changed (shortened).
Development would still be required, but at least the tooling would be
in place for some of the major hardware.


Hmmmmmm.

"Stick/DIV".

S-DIV.

S-IVD?


Would they name the upper stage Delta V (aka delta-v)?

Brian
  #7  
Old September 8th 05, 02:37 AM
Pat Flannery
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Alex Terrell wrote:

Using a Delta IV common booster would save a lot of development work,
but that rather defeats the puropose of the Stick.



Not really- it has a lifting capability superior to the Delta 4 heavy
and gets the payload to orbit with a total of only two main engines
being fired (one solid, one liquid) which should boost reliability.

Pat
  #8  
Old September 8th 05, 05:19 AM
Reed Snellenberger
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"Ed Kyle" wrote in news:1126129461.850078.177030
@f14g2000cwb.googlegroups.com:

Has anyone else noticed that the proposed
SRB/SSME "Stick" vehicle has a second stage
diameter that is roughly the same as the
diameter of the Delta IV Common Booster
Core (5.1 meters)? And, by the way, that
the SRB/SSME second stage length seems to
be not much less than the length of a CBC?

- Ed Kyle


Accidents like that happen a lot in the space industry -- some people think
that Buran looks a lot like the Space Shuttle... :-)

--
I was punching a text message into my | Reed Snellenberger
phone yesterday and thought, "they need | GPG KeyID: 5A978843
to make a phone that you can just talk | rsnellenberger
into." Major Thomb | -at-houston.rr.com

  #9  
Old September 8th 05, 09:49 AM
Alex Terrell
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I mean the only purpose of the stick is to provide development work.
Hence White Elephant.

  #10  
Old September 9th 05, 07:42 PM
Tom Cuddihy
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Ed Kyle wrote:
Has anyone else noticed that the proposed
SRB/SSME "Stick" vehicle has a second stage
diameter that is roughly the same as the
diameter of the Delta IV Common Booster
Core (5.1 meters)? And, by the way, that
the SRB/SSME second stage length seems to
be not much less than the length of a CBC?

- Ed Kyle


also roughly the same diameter as the Falcon IX from SpaceX!
(yes, okay, fairing diameter, not core, and yes, spacex would probably
not want to work with a NASA integrated upper stage)


http://www.spacex.com/index.html?sec...%23reliability

But hey--maybe NASA's just looking for commonality across several
providers?

Tom

 




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