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DUAL-POLARIZED ANTENNA SYSTEM


Synopsis - Aug 27, 2008
Modification 01 - Posted on Oct 09, 2008

General Information
Solicitation Number: NNG08258756Q
Posted Date: Aug 27, 2008
FedBizOpps Posted Date: Aug 27, 2008
Original Response Date: Sep 17, 2008
Current Response Date: N/A
Classification Code: 59 -- Electrical and electronic equipment components
NAICS Code: 334511 - Search, Detection, Navigation, Guidance, Aeronautical, and Nautical System and Instrument Manufacturing

Contracting Office Address
 
NASA/Goddard Space Flight Center, Wallops Flight Facility, Code 210.W, Wallops Island, VA 23337

Description
 
NASA/GSFC plans to issue a Request for Quotations (RFQ) for the following Commercial item: Quantity of 1 Integrated S-Band (2700-2900 Mhz) dual-polarized antenna system. The antenna system shall consist of a parabolic reflector, dual-polarized feed horn, pedestal, drive motors, and servo-amplifiers. The system shall be capable of emitting and receiving both horizontal and vertical linearly polarized RF energy. The antenna system will be used as an integrated component of a transportable meteorological research radar, and all of the components, except the pedestal, shall be constructed so that they may be shipped in standard ISO seatainers with outside dimensions of either 2.44m x 2.44m x 6.1m (8' x 8' x 20') or 2.44m x 2.44m x 12.2m (8' x 8' 40'). The primary objective of the radar system is to collect meteorological research quality reflectivity, Doppler and polarimetric data at various locations in the world. The antenna system shall be capable of handling up to 1.0 megawatts peak pulsed power with pulse widths up to 2 microseconds and pulse recurrence frequencies up to 1200 pulses per second. The antenna will be scanned in the azimuth and elevation planes; it will not be used for closed loop tracking. The antenna-pedestal system will be designed to operate without a radome under wind, acceleration and environmental conditions as specified in the Statement of Work. A high performance antenna is required for accurate measurements of dual-polarimetric quantities. The electrical specifications of th feed/OMT, reflector surface accuracy and secondary patterns are hence stringent as specified in the Statement of Work. The Government will require a preliminary design review (PDR), a final design review (FDR), and range testing at which time the contractor will certify that all specifications have been met. Full acceptance by the Government will occur after contractor installs the antenna on the pedestal with precision alignment and demonstrates that the reflector surface accuracy satisfied < 0.02" rms.

The NAICS Code and Size Standard are 334511 and 750, respectively.

The anticipated release date of RFQ NNG08258756Q is on or about 09/17/2008 with an anticipated due date of on or about 10/17/2008.

All responsible sources may submit a Request for Quotation which shall be considered by the agency.

An ombudsman has been appointed. See NASA Specific Note "B". James A. Balinskas, Director of Contract Management Division and may be contacted at 202-358-0445 or email address: james.a.balinskas@nasa.gov.

The solicitation and any documents related to this procurement will be not be available over the Internet. These documents will be mailed to the Potential Quoters upon request.

Prospective offerors shall notify this office of their request for a copy of the RFQ. It is the offeror's responsibility to monitor the Internet site for the release amendments to this notice(if any).

All contractual and technical questions must be submitted in writing (e-mail or FAX) to Diana W. Frimmel, Code 210.W, NASA/Goddard Space Flight Center, Wallops Flight Facility, Wallops Island, VA 23337 not later than 9/11/2008. Telephone questions will not be accepted.


Point of Contact
Name:Diana W. Frimmel
Title:Contract Specialist
Phone:757-824-1290
Fax:757-824-1974
Email:Diana.W.Frimmel@nasa.gov

Name:Mickey Merritt
Title:Contract Officer
Phone:757-824-1592
Fax:757-824-1974
Email: Mickey.M.Merritt@nasa.gov

Government-wide Notes
NASA-Specific Notes
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