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COMMERCE BUSINESS DAILY ISSUE OF JUNE 15,2000 PSA#2622NASA/Goddard Space Flight Center, Code 214.3, Greenbelt, MD 20771 A -- ENERGETIC PARTICLE DETECTOR FOR NASA/GSFC ST-5 MISSION DUE 070500
POC James S. King, Contracting Officer, Phone (301) 286-2533, Fax (301)
286-0383, Email James.S.King.1@gsfc.nasa.gov -- Hettie Courtney,
Contracting Officer, Phone (301) 286-8124, Fax (301) 286-0383, Email
Hettie.S.Courtney.1@gsfc.nasa.gov WEB: Click here for the latest
information about this notice,
http://nais.msfc.nasa.gov/cgi-bin/EPS/bizops.cgi?gr=D&pin=51#RFI-07050
0-303. E-MAIL: James S. King, James.S.King.1@gsfc.nasa.gov. NASA/GSFC
is hereby soliciting information from potential sources for an
energetic particle detector (EPD) to be flown aboard the six-month ST-5
Mission which is scheduled to launch in May 2003. The formal
requirements and specifications for this instrument are currently being
developed, but general characteristics of the instrument are as
follows: ENERGETIC ION AND ELECTRON SPECTROMETER- Mature instrument
(i.e., possessing flight heritage, with development limited to
packaging/interface requirements); ion and electron spectrometer using
solid-state and/or time-of-flight technology; mounted on spinning
spacecraft (20 rpm; spin axis normal to plane of ecliptic) in ~200 km
x ~35,786 km altitude orbit (i.e., GTO); minimum lifetime three months;
radiation tolerant (100 krads total dose); operate from 5 volt
spacecraft power bus; three flight units and one spare required.
UTILIZATION- Characterization of high altitude energetic charged
particle substorm injection events at altitudes above 25,000 km.
FUNCTIONAL REQUIREMENTS- Minimum energy ranges: Ions 100 keV to 1 MeV,
and Electrons 100 keV to 500 keV; energy resolution: <25%; mass
analysis desireable, but not required; Particle Anisotropy in the plane
of the ecliptic to be determined by sectored sampling synchronized to
spacecraft spin phase; some measurement of angular dependence of
particle flux out of the ecliptic is desireable, but not required.
RESOURCES- Mass: ~1.5 kg; Power: ~1.5 W; Telemetry rate: ~1 kbps (orbit
averaged). NASA/GSFC is interested in responses regarding both the
industry capability/product availability to satisfy this requirement
(in the form of documentation, literature, brochures, and references),
as well as comment on the technical requirements as described above
(feasibility, etc). Responses can be submitted by electronic mail to
the primary POC, James King, designated below, or submitted by mail, to
Mr. King, at the designated Contracting Office address. No solicitation
exists; therefore, do not request a copy of the solicitation. If a
solicitation is released it will be synopsized in the CBD and on the
NASA Acquisition Internet Service. It is the potential offerors
responsibility to monitor these cites for the release of any
solicitation or synopsis. Tentatively, GSFC envisions the synopsizing
of a solicitation shortly after receipt and evaluation of responses to
this RFI. Please advise if the requirement is considered to be a
commercial or commercial-type product. A commercial item is defined in
Internet "Note A". This synopsis is for information and planning
purposes and is not to be construed as a commitment by the Government
nor will the Government pay for information solicited. Respondents will
not be notified of the results of the evaluation. Respondents deemed
fully qualified will be considered in any resultant solicitation for
the requirement. Any referenced notes can be viewed at the following
URL: http://genesis.gsfc.nasa.gov/nasanote.html Posted 06/13/00
(D-SN464250). (0165) Loren Data Corp. http://www.ld.com (SYN# 0015 20000615\A-0015.SOL)
A - Research and Development Index Page
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