SOLICITATION NOTICE
66 -- MAI-400C ADACS SYSTEM
- Notice Date
- 10/21/2014
- Notice Type
- Combined Synopsis/Solicitation
- NAICS
- 334511
— Search, Detection, Navigation, Guidance, Aeronautical, and Nautical System and Instrument Manufacturing
- Contracting Office
- NASA/Goddard Space Flight Center, Code 210.Y, Greenbelt, MD 20771
- ZIP Code
- 20771
- Solicitation Number
- NNG14527979Q
- Response Due
- 10/30/2014
- Archive Date
- 10/21/2015
- Point of Contact
- Gilser A Nash, Purchasing Agent, Phone 301-286-4926, Fax 301-286-5373, Email Gilser.A.Nash@nasa.gov
- E-Mail Address
-
Gilser A Nash
(Gilser.A.Nash@nasa.gov)
- Small Business Set-Aside
- N/A
- Description
- NASA/GSFC has an requirement for Attitude Determination and Control System (ADCS) for the IceCube Cubesat project. The soecifications for the ADCS are as follows: - The unit will fit into a volume defined as 10cm x 10cm x 6.7cm - The unit will weigh less than 0.85 kg - The unit will contain channels for feed through of cables - The data interface for the unit will be a asynchronous serial interface conforming electrically to either RS-232 or TTL UART - The unit will be powered with 5V and/or 12V - The unit will contain performance attitude determination of the spacecraft using at a minimum: coarse sun sensors, fine sun sensor and three axis magnetometer (TAM) - The unit will be capable of interfacing with an SSBV Digital Fine Sun Sensor - The unit will either interface to a provided external TAM or include a TAM internally - The unit will be capable of accepting and determining sun angle from six analog coarse sun sensors and have tuning parameters for calibration of the sun sensor outputs - The unit will be capable of better than 0.5 deg attitude knowledge accuracy using the combination of the SSBV fine sun sensor and TAM - The unit will control the attitude using a three axis stabilization scheme using three reaction wheels and three magnetic torque rods for dumping reaction wheel momentum - The unit will contain three reaction wheels capable of storing at least 10 mNms - The unit will contain three magnetic torque rods capable of dipole moments of at least 0.1 Am^2 - The unit will be capable of better than 1 deg attitude control accuracy using reaction wheels and attitude solution based on the SSBV fine sun sensor and TAM - The unit will have a momentum dumping algorithm which utilizes the magnetic torque rods to actively dump momentum from the reaction wheels - The unit will have an orbit propagator which will accept ephemeris updates messages or directly read a Novatel OEM615 GPS receiver - The unit will have a control mode for detumble that uses only the magnetic torquers and TAM - The unit will have a control mode for pointing any axis to the sun with the ability to spin about the sun vector at a commanded "rotisserie" rate between 0.2 and 1 revolutions per minute In addition to providing the unit below, support during initial orbit acquisition and check out of the spacecraft will also be required for the unit. This includes attitude determination, ADCS unit health as safety assessment, dynamic analysis, troubleshooting and "green for science operations" assessments. The support needed will not exceed 40 hours. This notice is a combined synopsis/solicitation for commercial items prepared in accordance with the format in FAR Subpart 12.6, as supplemented with additional information included in this notice. This announcement constitutes the only solicitation, which is issued as a Request for Quotation (RFQ); quotes are being requested and a written solicitation will not be issued. Offerors are required to use the On-Line RFQ system to submit their quote. The On-line RFQ system is linked above or it may be accessed at http://prod.nais.nasa.g ov/cgi-bin/eps/bizops.cgi?gr=C&pin=. The information 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 Simplified Acquisition Procedures set forth in FAR Part 13. Questions regarding this acquisition must be submitted in writing (e-mail is preferred) no later than October 24, 2014. It is the quoter's responsibility to monitor this site for the release of amendments (if any). Potential quoters will be responsible for downloading their own copy of this notice, the on-line RFQ and amendments (if any). NASA Clause 1852.215-84, Ombudsman, is applicable. The Center Ombudsman for this acquisition can be found at http://prod.nais.nasa.gov/pub/p ub_library/Omb.html.
- Web Link
-
FBO.gov Permalink
(https://www.fbo.gov/spg/NASA/GSFC/OPDC20220/NNG14527979Q/listing.html)
- Record
- SN03554861-W 20141023/141021234315-b000996b5329159a4967a4d44e6208b8 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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