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Sent: Thursday, November 08, 2001 12:26 PM
Subject: Clinton ISS Policies Largely Caused ISS Cost Overruns


Click here: http://www.spaceref.com/docs/NASA/ISS/imce_appdx.pdf -Section
3.3 of this Young ISS Commission Apendix states that the budget caps placed
on the ISS by the Clinton Administration largely caused the present ISS cost
overruns.

Rick L. Sterling
____________________________________

WRONG!  Section 3.3 -- like the rest of the Young Report -- says flatly that
NASA (in this case, Dan Goldin) deliberately deceived the Clinton
Administration (as it had deceived the Reagan and Bush Sr. Administrations)
about what the Station as a whole would cost -- and that it did so by
"meeting" Clinton's yearly cost caps by simply delaying Station expenses
which it knew all along would be necessary into the future, until it finally
became impossible to conceal them any longer.  This is exactly what NASA had
done previously with the Shuttle -- and, from NASA's point of view, both
projects weren't "failures".  They were brilliantly successful at doing what
NASA intended both the Shuttle and the Station to do from the start: defraud
the taxpayers for decades before the deceptions were finally discovered.  As
science journalist Daniel S. Greenberg says, from the start NASA's cost
estimate for the Station was "sucker bait for gullible Congressmen".
Nowhere does the Young report blame Clinton: its blame is focused entirely
on NASA, and on NASA's deliberate (not accidental) deceptions.

But let me quote Section 3.3 of the Report in its entirety (it's very
short):

"Perhaps the single greatest factor in the cost growth of the ISS program
has been NASA's culture to manage the program in its annual budgets.  A the
time that the Clinton Administration and Congress approved the redesigned
Space Station [which, as the rest of the Report says, they would never have
done if Goldin hadn't falsely assured them that his redesign would vastly
cut its cost], annual budget caps of $2.1 billion were levied on the program
as a means to control costs.  In general, such caps establishing level
annual funding on a major program are counterproductive to controlling total
program cost.  Total cost and schedule became variables as NASA's focus
became one of executing the program within the annual budgets.  Additional
funding was requested and provided for the Russian Program Assurance and
Crew Return Vehicle; however, program content was continually slipped to the
right (and outside the 5-year budget windows) to stay within the annual
budget caps.

"Various budget exercises and shifting of resources have been employed to
maintain the annual budget caps.  In the period from Fiscal Year 1995
through FY 2001, $966 million in O&S [Operations and Support] funding and
$980 million in research funding were transferred to development within the
ISS budget line (based on the FY 2000 budget structure and the initial
funding levels provided in the FY 95 budget).  In 2000, Congress enacted a
new cap of $25 billion.  This cap is on the accumulated annual funding since
FY 94 until the year when the funding for development is less than 5% of
that year's budget.  At the same time, the ISS budget was restructured and
the 'Operations Capability and Construction' line was moved from development
to operations.  The estimated cost for this budget line in the FY 01 budget
through FY 05 was $878 million.  Finally, the FY 01 budget transferred
out-year funding of the Crew Return Vehicle totalling $765 million from the
ISS budget line in the Human Space Flight appropriation to a line in the
Science, Aeronautics and Technology appropriation.  Both of these budget
exercises are clearly associated with the new cap of $25 billion."

Now let me quote the first paragraph of Section 3.5 of the report ("Budget
Summary"):

"In summary, the original cost estimate was extremely optimistic.
Administator Goldin's management style of 'better, faster, cheaper'
permeated the program's redesign.  Every element of the Station was pushed
during the redesign phase to reduce costs.  Content that was removed during
redesign has fought its way back into the program."  [The Report goes into
great detail on the latter fact.]

This Report places the blame for the whole fiasco squarely on NASA's
shoulders -- and, as it points out, NASA's bookkeeping is still being kept
so deliberately sloppy to cover up the scheme that the Young Committee has
no real idea how much more the Station will end up costing than its current
minimal estimate of the cost overrun.  (For one thing, it points out in
Section 5.1.3 that it now looks as though even NASA's estimate that a 3-man
Station crew can do a piddling 20 hours per week of science research is a
serious overestimate.)  Sure, if earlier Administrations had given NASA
humongously more money to play with, the Station would have been built to
the capacity that NASA promised -- but then, if NASA had been honest about
the cost of the Station, the thing would never have been funded in the first
place.

But read the whole (quite brief and concise) Young Report for yourselves:
www.spaceref.com/docs/NASA/ISS/imce.pdf
www.spaceref.com/docs/NASA/ISS/imce_appdx.pdf

As for possible more economical designs for a Station, there were at least
two superb pieces on the subject all the way back during the first Bush
Administration, when the fraud was already clear for anyone to see (and when
Greenberg wrote his "sucker bait" comment).  One (Aviation Week, 1/13/92,
pg. 53) is "Veteran Designer Offers Reconfigurable Alternative to NASA Space
Station".  The other is aerospace historian T.A. Heppenheimer's detailed
program overview "Beyond Tomorrow: Realistic, Useful Alternatives to NASA's
Grandiose Space Station" in the May 1991 issue of the libertarian magazine
"Reason".  (Heppenheimer, by the way, is in no way a hard-line
libertarian -- there's not a speck of Ayn Randian fantasy in the article).

And as for the feasibility of Shuttle-C as a good future design for big
American boosters: Robert C. Truax -- who played a central role in
conceiving the Polaris missile, and then played Cassandra in the late
Seventies by prcisely but futilely predicting what the Space Shuttle would
turn into -- has a terrific piece on the optimal future design for big,
economical boosters in the January 1999 "Aerospace America" ("The Future of
Earth-to-Orbit Propulsion").  (Among many other things, he takes a dim view
of strap-on boosters.  His article spurred several letters to the magazine
by other aerospace engineers -- every one of whom completely agreed with
him, except for one who had studied pressure-fed engines in detail and
thought Truax had overestimated their preferability to turbopumps, because
tank walls capable of containing such higher pressures are thick and heavy.)

Rather than summarize these three articles -- and since two of them may be
almost impossible for non-American readers to find -- I'll insert all three
of them soon in the File Vault of the Astronautics Group.




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