Lou,

IMHO, the "poor management" problem does not only belong to NASA, also to the 
senate committee. The committee should help NASA improve their Verification and 
Qualification procedure.

Not long ago NASA had a failed mission due to a design mistake omitting 
transition unit for propelling force in Pound to Kilogram. Pretty soon they had 
the second failed mission. This time it is because "The software ... was not 
properly implemented" (see the NASA report below). 

Are all these overlook mistakes are forgivable to taxpayers?

Barry Ma
b...@anritsu.com
---------- Original Text ----------

From: "Lou Gnecco" <l...@tempest-inc.com>, on 3/30/00 2:20 PM:


Sen. McCain is on the committee that oversees NASA. He recently said that the 
basic problem is poor management. IMHOP he's right.
lou

--------------

Scott Lacey

Below is an excerpt from the complete NASA report. 

<<Premature shutdown of descent engines.
PLAUSIBLE. A magnetic sensor is provided in each of the three landing legs to 
sense touchdown when the lander contacts the surface, initiating the shutdown 
of the descent engines. Data from MPL engineering development unit deployment 
tests, MPL flight unit deployment tests, and Mars 2001 deployment tests showed 
that a spurious touchdown indication occurs in the Hall Effect touchdown sensor 
during landing leg deployment (while the lander is connected to the parachute). 
The software logic accepts this transient signal as a valid touchdown event if 
it persists for two consecutive readings of the sensor. The tests showed that 
most of the transient signals at leg deployment are indeed long enough to be 
accepted as valid events, therefore, it is almost a certainty that at least one 
of the three would have generated a spurious touchdown indication that the 
software accepted as valid.  The software - intended to ignore touchdown 
indications prior to the enabling of the touchdown sensi!
!
ng logic - was not properly implemented, and the spurious touchdown indication 
was retained. The touchdown sensing logic is enabled at 40 meters altitude, and 
the software would have issued a descent engine thrust termination at this time 
in response to a (spurious) touchdown indication.
MOST PROBABLE CAUSE OF LOSS OF MISSION>>


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