NASA/Dryden Flight Research Center, Code A, P.O. Box 273, Edwards, CA 93523-0273

58 -- FLIGHT TERMINATION COMMAND RECEIVER/DECODER SOL RFO-P82900061-CLV DUE 012698 POC Carol L. Van Gelder, Contracting Officer, Phone (805) 258-3071, Fax (805) 258-2904, Email carol.van.gelder@qmgate.dfrc.nasa.gov WEB: Click here for the latest information about this notice, http://procurement.nasa.gov/EPS/DFRC/date.html#RFO-P82900061-CLV. E-MAIL: Carol L. Van Gelder, carol.van.gelder@qmgate.dfrc.nasa.gov. NASA/DFRC plans to issue a Request for Offer (RFO) for Flight Termination Command Receiver/Decoder, shall meet RCC 319-92 Flight Termination Systems Commonality Standard. Units shall have the input/output functions as shown in TABLE 1. TABLE 1-FUNCTION STANDARD/FAILSAFE: +28 VDC Power; No Connection; DC Return; DC Return; DC Return; DC Return/Failsafe Enable; No Connection; Terminate Commands; No Connection; Optional Command; No Connection/Low Voltage Sense; Tune Monitor C; Case Ground; +28 VDC Power; No Connection; Tone Monitor B; Tone Monitor A; DC Return; No Connection; Terminate Command; No Connection; Monitor Command; Arm Command; Signal Strength; Signal Strength Return. Units shall meet the following Environmental requirements and Test Data pack shall be provided with each unit. ENVIRONMENTAL (QUALIFICATION TEST LEVELS): Electromagnetic Interference: The unit is designed to meet the requirements of MIL-STD-461C, for Class A equipment with the following changes; CS04 Conducted susceptability; 10MHz to 8.5 GHz, 60 dB minimum RF level; Specific Band Rejection >100 dB: 2.2 to 2.4, 5.4 to 5.9, 9.4 to 9.8 GHZ. Operating Temperature: The unit meets all electrical requirements over a temperature range of -54 degrees centigrade to +85 degrees centigrade. Humidity: 0 to 97% relative. Shock: 1100 g's half-sine, 5 mS; 100 g's saw tooth, 11 mS. Random Vibration: 18.6 g's rms for one hour; 30 g's rms for 10 min., 3 axis. Altitude/Temperature: 250,000 feet at -40 degrees centigrade. Pressure: 30 lb/in- for 30 minutes. Acceleration: 118 g's, 5 minutes, 3 Axis. Derating: MIL-STD-975 is used as a guideline for derating of all components. Mechanical Dimensions: Shall be 1.0"x2.20"x3.30" or smaller. Weight: 8 ounces, maximum. This procurement is being conducted under the NASA MidRange Pilot Test Program approved by the Office of Federal Procurement Policy. The Government intends to acquire a commercial item using FAR Part 12. This procurement is a total small business set-aside. See Note 1. The SIC Code and Size Standard are 3823 and 1000 employees, respectively. The DPAS Rating for this procurement is DO-C9. The provisions and clauses in the RFO and model contract are those in effect through FAC 97-2. All qualified responsible sources may submit an offer which shall be considered by the agency. The anticipated release date of the RFO is on or about December 21, 1997 with an anticipated offer due date of on or about January 26, 1998. An ombudsman has been appointed. See Internet Note "B". The solicitation and any documents related to this procurement will be available over the Internet. These documents will be in Microsoft Office Suite (Word 6.0, Excel 5.0, PowerPoint 4.0) format and will reside on a World Wide Web (WWW) server, which may be accessed using a WWW browser application. The WWW address, or URL of the NASA/DFRC Business Opportunities home page is http://procurement.nasa.gov/EPS/DFRC/class.html. Prospective offerors shall notify this office of their intent to submit an offer. It is the offeror's responsibilityto monitor this site and/or the CBD for the release of the solicitation and amendments (if any). Potential offerors will be responsible for downloading their own copy of the solicitation and amendments (if any). Any referenced notes can be viewed at the following URL: http://genesis.gsfc.nasa.gov/nnotes.htm. (0337)

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