A Space & astronomy forum. SpaceBanter.com

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

Apollo Style Escape Tower Question....



 
 
Thread Tools Display Modes
  #11  
Old January 13th 04, 03:14 AM
Jorge R. Frank
external usenet poster
 
Posts: n/a
Default Apollo Style Escape Tower Question....

"Keith F. Lynch" wrote in
:

Henry Spencer wrote:
(Mercury had a much more comprehensive automatic escape system, and
debugging it had been a nightmare. So for Apollo, automation was
confined to the one case where fractions of a second counted.)


Was it a Mercury or a Gemini mission where the rules called for an
eject, but the astronaut(s) correctly guessed that the rocket hadn't
actually left the pad, as the instruments claimed it had? That
obviously wasn't automated.


Gemini 6 (Schirra/Stafford):

http://www.astronautix.com/flights/gemini6.htm

--
JRF

Reply-to address spam-proofed - to reply by E-mail,
check "Organization" (I am not assimilated) and
think one step ahead of IBM.
  #12  
Old January 13th 04, 04:17 AM
Pat Flannery
external usenet poster
 
Posts: n/a
Default Apollo Style Escape Tower Question....



Keith F. Lynch wrote:

Was it a Mercury or a Gemini mission where the rules called for an
eject, but the astronaut(s) correctly guessed that the rocket hadn't
actually left the pad, as the instruments claimed it had? That
obviously wasn't automated.

Gemini 6; Gemini used a manual abort system. Mercury was entirely
automatic; Apollo's was a combo manual/automatic system.

Pat

  #13  
Old January 16th 04, 11:28 PM
Eric Pederson
external usenet poster
 
Posts: n/a
Default

Reed Snellenberger wrote:

Richard Stewart wrote in
news

Fair enough - so if our theoretical rocket stack (stack plus two solid
rocket boosters) had an O ring burn through (a la Challenger) as soon
as the stack broke up and/or veered fractionally off center rapidly
enough, the escape rockets would get the capsule otta there! Hopefully
far enough & fast enough away that debris/explosion doesn't pose a
hazard...


Solids probably won't be a factor in any more manned launchers due to the
possibility of a catastrophic failure in the motor. There are videos of
both Delta II & Titan 34D launches in which the transition from launcher
to fragments occurs within a video frame. It's unlikely that even an
automated system could react quickly enough in that situation. The
advantage of liquid-fueled systems is that most problems in the motors
can be contained, at least briefly, allowing the escape systems time to
activate.

--
Reed


Oddly, the exception to that rule will be the escape system.
  #14  
Old January 19th 04, 07:58 PM
Scott Hedrick
external usenet poster
 
Posts: n/a
Default


"Hallerb" wrote in message
...
One
good rason to retire the shuttle...


"rason"? Is that what particles the Zeta Reticulans shoot out of their ray
guns?


 




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
Moon key to space future? James White Policy 90 January 6th 04 04:29 PM
Apollo vehicle sequence question Charles Buckley History 3 December 28th 03 04:58 PM
Apollo Hypothetical Question (CSM Tracking) Jonathan Silverlight History 12 October 6th 03 04:25 PM
Apollo 7 Saturn Question pjo History 10 September 22nd 03 01:21 AM
If Liberty bells hatch hadnt blown? Hallerb History 28 August 30th 03 02:57 AM


All times are GMT +1. The time now is 12:34 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2024, Jelsoft Enterprises Ltd.
Copyright ©2004-2024 SpaceBanter.com.
The comments are property of their posters.