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FBO DAILY ISSUE OF JANUARY 29, 2005 FBO #1160
MODIFICATION

66 -- STRAIN AND MOTION ANALYSIS SYSTEM

Notice Date
1/27/2005
 
Notice Type
Modification
 
NAICS
334516 — Analytical Laboratory Instrument Manufacturing
 
Contracting Office
NASA/George C. Marshall Space Flight Center, Procurement Office, Marshall Space Flight Center, AL 35812
 
ZIP Code
35812
 
Solicitation Number
NNM05097423Q
 
Response Due
1/31/2005
 
Archive Date
1/27/2006
 
Point of Contact
Marianne R. Campbell, Contract Specialist, Phone (256) 544-6496, Fax (256) 544-9080, Email marianne.campbell@msfc.nasa.gov - Betty C. Kilpatrick, Contract Specialist, Phone (256) 544-0310, Fax (256) 544-6062, Email betty.c.kilpatrick@nasa.gov
 
E-Mail Address
Marianne R. Campbell
(marianne.campbell@msfc.nasa.gov)
 
Description
THIS NOTICE CONSTITUTES AMENDMENT NO. 1 TO THE COMBINED SYNOPSIS/RFQ FOR STRAIN AND MOTION ANALYSIS SYSTEM. Companies shall acknowledge all amendment(s) in their quote. This notice serves as the official amendment to subject synopsis/RFQ and a written amendment will not be issued. The purpose of this amendment is to Answer questions asked before the due date of proposals. 1. Question: Will the shearography system work with the high speed camera? Do you want to measure the deformations and deflections of the structures during the firing test? Or do you want a more ordinary EPSI or shearography system? Answer: The shearography system will not be used with the high-speed video. It will be used with a 2 watt solid state laser that is supplied with the system. The shearography will not be used during the firing tests but may be required to support some investigative testing on the frangible nuts or hold-down studs. Two measurements from the high-speed video will shoot during the firing tests. This data will be post processed from 10 high-speed digital video cameras. One measurement to be performed is to quantify strain information from the frangible nut while the explosive charge is fracturing the nut. The other measurement to be performed will be to track the nut halves as they move away after fracture. This tracking information will include trajectory and velocity plots. 2. Question: What kind of installation timeline is required? Answer: The successful vendor will be on site for 2 weeks to operate the system for our first series of tests and train one of our engineers in the use of the system. The testing will begin February 7 so every piece of hardware must be shipped in and processed through our property management system to support that date. The due date for receipt of offers is not extended. Companies shall provide the information stated in the synopsis/RFQ posted on the NASA Acquisition Internet Service (NAIS) on January 25, 2005. Documents related to this procurement are available over the Internet. These documents reside on a World Wide Web (WWW) server which may be accessed using a WWW browser application. The Internet site, or URL, for the NASA/MSFC Business Opportunities home page is http://prod.nais.nasa.gov/cgi-bin/eps/bizops.cgi?gr=D&pin=62 NOTE: THIS NOTICE WAS NOT POSTED TO WWW.FEDBIZOPPS.GOV ON THE DATE INDICATED IN THE NOTICE ITSELF (27-JAN-2005); HOWEVER, IT DID APPEAR IN THE FEDBIZOPPS FTP FEED ON THIS DATE. PLEASE CONTACT fbo.support@gsa.gov REGARDING THIS ISSUE.
 
Web Link
Click here for the latest information about this notice
(http://www.eps.gov/spg/NASA/GMSFC/POVA/NNM05097423Q/listing.html)
 
Record
SN00741755-F 20050129/050127214405 (fbodaily.com)
 
Source
FedBizOpps.gov Link to This Notice
(may not be valid after Archive Date)

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