[net.space] Shuttle Computers and STS power consumption

@S1-A.ARPA,@MIT-MC.ARPA:jim@TYCHO.ARPA (06/19/85)

From: jim@TYCHO.ARPA    (James B. Houser)


        A recent posting about  shuttle  cooling  reminded  me  of  an
article  I  ran  across  in  an  old (1980) IBM document.  The article
described the onboard computers as System/4Pi model AP-101 processors.
The  AP-101  appears  to  be  a  3  KIP machine with an intensely ugly
architecture.  Main memory was described as 104KW  (36  bit)  of  core
(really  core!)  with  400  ns access time.  What startled me were the
physical characteristics.  Each of the five  "processors"  appears  to
consist  of  two  boxes.  The  boxes  weigh  58.9  pounds and draw 350
Watts!!!!! This would imply a system total of almost  600  pounds  and
3500  Watts.  Did  they actually use this refugee from the Smithsonian
on the Shuttle and if so are  there  any  reasonable  plans  afoot  to
upgrade?  In  a  related  question, what are the major contributors of
heat during the orbital portion of a shuttle mission?


-------

arnold@ucsfcgl.UUCP (Ken Arnold%CGL) (06/21/85)

In article <2322@mordor.UUCP> @S1-A.ARPA,@MIT-MC.ARPA:jim@TYCHO.ARPA writes:
>A recent posting about shuttle cooling reminded me of an article I ran
>across in an old (1980) IBM document.  The article described the
>onboard computers as System/4Pi model AP-101 processors.  The AP-101
>appears to be a 3 KIP machine with an intensely ugly architecture.
>Main memory was described as 104KW (36 bit) of core (really core!)
>with 400 ns access time. ...  Did they actually use this refugee from
>the Smithsonian on the Shuttle and if so are there any reasonable
>plans afoot to upgrade?

One of the main problems with space ship design is that, by the time
the design sits on the launching pad, its technology is quite out of
date.  This is true of all technology, but since computer technology
evolves considerably faster than other kinds, it is much more critical
(as the above description shows).

The California Space Resources institute (attached to the University of
California at San Diego) is currently coordinating a study which
includes this problem, relating the design of the space station.  As I
understand it, the problem is to define computer (and where possible
other techonological) needs by interface, and maximum physical
attributes (which, as things get smaller and generate less heat,
becomes not much of a problem); basically a form of modular technology
design.  That's what seemed most promising last time I was informed,
but it has been several months.

As an aside, in case you've been wondering where your defense dollars
are going, the same problem exists in front line equipment, which takes
just as long to get to the front.  Of course, the degree to which
computers are out of date varies among different pieces of equipment.

		Ken Arnold

ken@hrpd3.UUCP (K.COCHRAN) (06/21/85)

Could the use of core memory have anything to do with data
integrity when cosmic rays pass through the shuttle, or if
power drops unexpectedly.
				Ken Cochran   vax135!hr1ar!ken

al@aurora.UUCP (Al Globus) (06/27/85)

> 
>         A recent posting about  shuttle  cooling  reminded  me  of  an
> article  I  ran  across  in  an  old (1980) IBM document.  The article
> described the onboard computers as System/4Pi model AP-101 processors.
> The  AP-101  appears  to  be  a  3  KIP machine with an intensely ugly
> architecture.  Main memory was described as 104KW  (36  bit)  of  core
> (really  core!)  with  400  ns access time.  What startled me were the
> physical characteristics.  Each of the five  "processors"  appears  to
> consist  of  two  boxes.  The  boxes  weigh  58.9  pounds and draw 350
> Watts!!!!! This would imply a system total of almost  600  pounds  and
> 3500  Watts.  Did  they actually use this refugee from the Smithsonian
> on the Shuttle?

I'm almost positive the answer is yes, they do and will continue to
do so for the forseeable future.  If it's not that particular
model, it is a close relative.  Sickening isn't it?

Software note: software development for launch is supposedly very close
to the critical path and definitely must see major improvements to support
24 launches a year.

More horrors: there are some 250 microprocessors on the shuttle with a
variety of incompatable languages, operating systems, and development
systems between them.