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Notice Date
Notice Type
Combined Synopsis/Solicitation
334511 — Search, Detection, Navigation, Guidance, Aeronautical, and Nautical System and Instrument Manufacturing
Contracting Office
NASA/Dryden Flight Research Center, Code A, P.O. Box 273, Edwards, CA 93523-0273
ZIP Code
Solicitation Number
Response Due
Archive Date
Point of Contact
Cynthia Garcia, Contracting Officer, Phone 661-276-2592, Fax 661-276-2904, Email Cynthia.M.Garcia@nasa.gov - Gail Anton, Acquisition Support Specialist, Phone 661-276-5417, Fax 661-276-2243, Email gail.anton-1@nasa.gov
E-Mail Address
Cynthia Garcia
Small Business Set-Aside
NASA/DFRC has a requirement for qty: 4 Military ATR Chassis qty: 4 Chassis MountingTrayThe specifications are: ATR chassis specifications:Part Description:3/4 ATR, 7 Slot military Chassis Flowthrough Air CooledMilitary VME64x BackplaneThe back side of J0, J2 shall have long pins, by VMEbus specifications, and have pinshrouds installed Auto range & Auto frequency military PSU with 90-264VAC & 40-800Hz Input Power, 500 WattsOutput Power Extra 3.3VDC 45 Amps DC/DC converter-6Uboard fitted and wired in backplane slot 7High Profile Top Cover with 35 mm of top clearance, High profile Bottom Cover with 50 mmof bottom clearanceOne 115VAC & 65 CFM Rotron rear military Fan fitted for auto voltage & frequency throughan Electronics Converter Box, EMI/EMC fingerguard, Chassis Black color, reference designators and legends in contrasting (preferred white) colorFront connector panel layout will follow NASA requirements and consist of the followingMIL-C-38999 uniquely keyed connectors:J1: D38999/20FJ35SNJ2: D38999/20FE35SNJ3: D38999/20FJ35SAJ4: D38999/20FH35SNJ5: D38999/20FE35SAJ6: D38999/20FJ35SBJ7: D38999/20FJ35SBJ8: D38999/20FE06PNJ9: D38999/20FJ35SCBase dimension of the chassis in mm: 170.0 x 236.0 x 390.0 plus the required height ofthe top and bottom covers.Front panel LED indicators: ON, SYSFAIL (SYSF), ACFAIL (ACF), & VME (when there is datatransfer activity on the VMEbus.Provide ARINC-404 front panel mounting hooks (NAS-622CT3) and rear panel pin receptaclesto use with the mounting tray.The chassis can be hard mounted or mounted on a shock-isolated tray.Meet MIL-STD-5400 equipment class 1A requirementsChassis Environmental SpecificationsMIL-STD-810F Temperature-55 to +80 degree C Operating-55 to +100 degree C StorageMIL-STD-810F AltitudeUp to 65,000 ft operatingMIL-STD-810F ShockSawtooth pulse 40g 11 msMIIL-STD-810F AccelerationUp to 12g, 3 axesMIL-STD-810F Humidity0-95%MIL-STD 461E EMI & EMCCE101, CE102, CS101, CS114, CS115, CS116, RE102, RE103, RS103Mounting Tray:Mounting Tray for chassis shall incorporate two hold-down devices (load limiting) and 4mounting platforms for installing shock absorbers and a set of chassis stainless steelhook plates.Other requirementsA complete set of MIL-STD-461E and MIL-STD-810F certificates shall be issued byindependent labs to be delivered with each chassisThis is a replacement for an existing chassis and it is required to have exact chassislayout and physical dimensions with the existing one to be interchangable. Seeinformation provided in contract.All chassis parts are precision machined by CNC in aeronautical aluminum in order toachieve an ultra lightweight metal structure with no burrs or sharp edges, and corrosionprotective external and internal finishes throughout.All aluminum surfaces are MIL-C-5541E chemical coated for corrosion resistance andelectrical conductivitySidewalls and rear panel are externally pinned without sacrificing ruggedness orcompromising EMI or environmental requirementsAll removable surfaces are equiped with integral EMI gasketsFront panel have retractable carrying handlesAll finishes are fungus resistantThree layer of external military epoxy paintEach product delivered shall pass inspections and testsChassis ManualsThis notice is a combined synopsis/solicitation for commercial items prepared inaccordance with the format in FAR Subpart 12.6, as supplemented with additionalinformation included in this notice. This announcement constitutes the onlysolicitation, which is issued as a Request for Quotation (RFQ); quotes are beingrequested and a written solicitation will not be issued. Offerors are required to usethe On-Line RFQ system to submit their quote. The On-line RFQ system is linked above orit may be accessed at http://prod.nais.nasa.gov/cgi-bin/eps/bizops.cgi?gr=C&pin=. Theinformation required by FAR Subpart 12.6 is included in the on-line RFQ.The Government intends to acquire a commercial item using FAR Part 12 and the SimplifiedAcquisition Procedures set forth in FAR Part 13.Questions regarding this acquisition must be submitted in writing (e-mail is preferred)no later than 4:30 p.m local time on May 27, 2010.Quotes/Proposal are due no later than4:30 p.m local time on June 1, 2010. It is the quoter's responsibility to monitor thissite for the release of amendments (if any). An ombudsman has been appointedAny referenced notes may be viewed at the following URLs link below.
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