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COMMERCE BUSINESS DAILY ISSUE OF JUNE 27,1997 PSA#1876NASA/John F. Kennedy Space Center, Procurement, Kennedy Space Center,
FL 32899 34 -- SEEKING INDUSTRY SOURCES AND INPUT ON THE PROCUREMENT OF A
THERMAL VACUUM CHAMBER FOR INSTALLATION AT THE KENNEDY SPACE CENTER
(KSC) DUE 071697 POC Mitch Colvin, Contracting Officer, Phone (407)
867-7230, Fax (407) 867-2042, Email Mitch.Colvin-1@kmail.ksc.nasa.gov
WEB: Click here for the latest information about this notice,
http://procurement.nasa.gov/EPS/KSC/date.html#151533. E-MAIL: Mitch
Colvin, Mitch.Colvin-1@kmail.ksc.nasa.gov. For planning purposes only
KSC is asking those firms with demonstrated experience in performing
similar projects (size, capability, etc.) to provide their
qualifications and previous experience related to the project scope
described below. Your comments on the design, construction and
procurement methodology to be used to procure a THERMAL VACUUM CHAMBER
for KSC are solicited. The project will consist of a thermal vacuum
chamber, facility to house the vacuum chamber and extension of existing
utilities at KSC to support operation of the facility. The scope of
this project is estimated to be within the range of 35 to 60 million
dollars. This project is not currently funded but the current program
schedule calls for construction to be initiated in early 1999. Please
limit your comments to the scope of work listed below. Project Scope:
The chamber will be located on Kennedy Space Center, Florida. The size
of the thermal vacuum chamber interior is approximately 15 meters high
by 15 meters wide by 33 meters long. A new structure, housing the
chamber, is included within the project. The Thermal Vacuum Chamber
shall meet the following requirements: 1) Clear interior space of 15
meters wide by 15 meters high by 33 meters long. The object to be
placed within the chamber is cylindrical. Thus a mailbox, square or
round shaped chamber will be considered. 2) The vacuum requirements are
10-8 torr when the chamber is empty, clean, and dry. 3) The chamber
will be used to simulate environments on other planets and will be
required to maintain pressures between 10-8 torr and atmospheric. The
atmosphere in the chamber may be composed of various gases (carbon
dioxide, nitrogen, argon, oxygen and water). 4) The main access door
(full width and height of the chamber) will open directly into a class
100,000 clean room. The movement of the access door will be to the
right or left of the chamber, a vertical lift door is not acceptable.
5) The interior of the chamber including shell and fixtures is to be
constructed of 304L or 316L stainless steel. 6) The chamber shall be
designed, constructed, tested and code stamped per ASME Section VIII
division 1 or 2. 7) The floor of the chamber shall be conductive and
air bearing pallet compatible. 8) The chamber shall have the capability
to simulate levels of solar radiation. The anticipated maximum level is
800 watts per meter squared. 9) A redundant control system for the
thermal chamber shall be designed to allow independent control of the
thermal and vacuum characteristics of the chamber. The system shall be
PC based. 10) The chamber design shall include a thermal system
capable of producing a radiating surface temperature range from -250
degrees F to +250 degrees F. The chamber may be filled with mixtures of
gas (see 3 above) surrounding the test object. The thermal system shall
be capable of maintaining the gas temperature between -220 degrees F
and +70 degrees F. 11) The chamber shall have access panels to allow
the test object to be connected to fluids, power and data transmission
lines to allow the object to be operated while in the chamber. 12) The
facility will be equipped with an uninterruptible power supply to
support an orderly shut down of the test operation in the event of
failure of primary power. The building to house the chamber is included
within this project. The building will include a control room, chamber
and mechanical/electrical equipment room. The minimum size of the
control room is 20 feet by 40 feet. The building area at the entrance
to the thermal vacuum chamber will be a class 100,000 clean room, the
remainder of the occupied building will be heated and air-conditioned.
All gases and liquid nitrogen piping and storage vessels are included
within this project. Storage vessels will be located exterior to the
building. KSC is seeking industry's response to the following three
approaches: A) NASA designs the project and the contractor with the
largest dollar amount of work within the contract is required to be the
prime contractor. B) Design/Build -- The contractor will provide design
and construction services for the project with NASA providing technical
criteria during the design process and limited design support and only
inspection services during construction. C) NASA procures the Facility
and Vacuum Chamber as separate contracts, with NASA integrating the
contracts into one project. Please comment on any other procurement
issues of concern to you. For example, would you prefer to have the bid
documents prepared as detailed plans and specifications or as a
performance specification? Industry is also encouraged to suggest
changes which would result in a better value to the government. For
example, if a change in size would result in using industry standard
sizes and still meet our requirements, thus, eliminating significant
labor costs to custom fabricate parts; or, changes in requirements
which would allow the use of readily available fabrication equipment.
A solicitation will not be issued as a result of this sources sought
synopsis. In the event funding is received for this project a synopsis
will be issued announcing the Governments intent to issue a
solicitation for the Thermal Vacuum Chamber. (0176) Loren Data Corp. http://www.ld.com (SYN# 0252 19970627\34-0003.SOL)
34 - Metalworking Machinery Index Page
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