NASA/DFRC has a requirement for quantity of 4 Military ATR Chassis and quantity of4 Chassis Mounting Tray. The specifications are:Part Description: 3/4 ATR, 7 Slot military Chassis Flow through Air Cooled Military VME64x Backplane The 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, 500Watts Output Power Extra 3.3VDC 45 Amps DC/DC converter-6Uboard fitted and wired in backplane slot 7 High Profile Top Cover with 35 mm of top clearance, High profile Bottom Cover with 50mm of bottom clearance One 115VAC & 65 CFM Rotron rear military Fan fitted for auto voltage & frequencythrough an Electronics Converter Box, EMI/EMC finger guard, Chassis Black color, reference designators and legends in contrasting (preferred white) color Front connector panel layout will follow NASA requirements and consist of the followingMIL-C-38999 uniquely keyed connectors:o J1: D38999/20FJ35SNo J2: D38999/20FE35SNo J3: D38999/20FJ35SAo J4: D38999/20FH35SNo J5: D38999/20FE35SAo J6: D38999/20FJ35SBo J7: D38999/20FJ35SBo J8: D38999/20FE06PNo J9: D38999/20FJ35SC Base 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 isdata transfer activity on the VMEbus. Provide ARINC-404 front panel mounting hooks (NAS-622CT3) and rear panel pinreceptacles to 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 Specifications MIL-STD-810F Temperatureo -55 to +80 degree C Operatingo -55 to +100 degree C Storage MIL-STD-810F Altitudeo Up to 65,000 ft operating MIL-STD-810F Shocko Saw tooth pulse 40g 11 ms MIIL-STD-810F Accelerationo Up to 12g, 3 axes MIL-STD-810F Humidityo 0-95% 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.This 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 4:30pm local time on August 11, 2010. Quotes/Proposal are due no later than4:30pm local time on August 16, 2010 It is the quoter's responsibility to monitor thissite for the release of amendments (if any). Potential quoters will be responsible fordownloading their own copy of this notice, the on-line RFQ and amendments (if any).An ombudsman has been appointed - See NASA Specific Note "B".Any referenced notes may be viewed at the following URLs link below.

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