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COMMERCE BUSINESS DAILY ISSUE OF MAY 19,1997 PSA#1848U.S. Department of Energy, Oakland Operations Office, 1301 Clay Street,
Room 700N, Oakland, CA 94612-5208 18 -- A PROGRAM RESEARCH AND DEVELOPMENT ANNOUNCEMENT FOR NEW CLASSES
OF RADIOISOTOPE POWER SYSTEMS AND RELATED TECHNOLOGIES POC Sandra R.
Silva, Contracting Officer, (510) 637-1878 NASA's plans for future
space and planetary surface mission call for small size spacecraft,
landers and robotic explorers. These future missions power requirements
cannot be met by the current (nominal 300 watt electrical) General
Purpose Heat Source- Radioisotope Thermoelectric Generator (GPHS-RTG).
Future mission requirements must be met by new technology Radioisotope
Power systems (RPS) having electrical power outputs in the three ranges
(30 to 150 milliwatts, 5 to 20 watts, and 100 to 200 watts) while
maximizing conversion efficiency and other desirable RPS attributes:
i.e., long lift (15 year missions), and the ability to withstand launch
and space environments. In addition, there is a requirement for
improvement for the one watt thermal Radioisotope Heater Unit (RHU)
used for thermal control of items such as electronic packages,
batteries and scientific instruments. Development of new units at the
1 to 10 watt heat levels will also be required. In both cases
development of reducedmass and volume packaging systems, while
maintaining or enhancing nuclear safety, is desirable. The Department
of Energy intends to issue a Program Research and Development
Announcement (PRDA) soliciting proposals for new, innovative energy
conversion concepts and cutting edge technologies and for furthering
the performance of promising current conversion technologies. Proposals
are also solicited for improved packaging systems for radioisotope fuel
sources in the three power level ranges which maintain or improve the
current GPHS nuclear flight safety margins. Proposals are solicited in
the following areas: (1) RPS Power Conversion Technologies (a)
Conceptual design of various high efficiency, low cost thermal to
electric type conversion systems within the three ranges specified. (b)
Prototypic component design, fabrication and performance/lift test for
developed conversion technologies. (2) New Radioisotope Heat Sources
Designs (a) Conceptual design for improved packaging systems for the
radioisotope heat sources in each of the three power level ranges,
supporting key safety analysis trade-off studies and proposed safety
verification testing plan. (3) New Heat Rejection System (a) Innovative
new designs for light weight, high efficiency heat rejection systems,
assessment of the application of new heat rejection systems to several
conversion systems and demonstration of fabrication feasibility and
performance. (4) New Materials Assessment and Development (a)
Assessment of the application of advanced materials, or proposed
studies for materials development, to enhance RPS and RHU performance
and endurance. Identification and assessment of critical materials
compatibility issues and performance/economic benefits. (5) New RPS
Power System Concepts (a) Conceptual design, performance prediction,
manufacture, performance/life testing of electrically heated
(simiulated radioisotope heat source) innovative new high efficiency
power systems or subsystems based on one of the indicated power ranges.
(6) New RHU Designs (a) Innovative, safe and light weight designs for
one, five and ten watt units. Potential RPS technologies or new
concepts may be in various stages of development. These phases are:
Phase I (up to 12 months with funding up to $300,000) comprises a
conceptual design, feasibility assessment, performance prediction and
demonstration plan for the proposed conversion technologies or
materials studies. Phase II (up to 16 months with funding up to
$600,000) comprises component/materials fabrication and performance
testing including, if applicable preliminary life/performance
degradation modeling. Phase III (up to 12 months with funding up to
$600,000) comprises extended life/performance testing, upgrade of
life/performance degradation modeling and technical transfer activity.
Offerors may submit proposals for one or more phases. Transition from
one phase to another will be at the option of DOE pending a review of
results of the effort to date and the availability of funding. This
PRDA is directed to universities and industry. Universities and private
industry may team with each other or, if applicable, with government
national laboratories. It is anticipated that up to one half of the
funding will be available for awards to universities. The solicitation
will be available for downloading on the Internet. Interested parties
may obtain a copy of the solicitation by accessing the Internet using
any Web browser, at the DOE Oakland Operations Office Home Page,
http://www.oak.doe.gov. No paper copies of the solicitation will be
made available. Prospective offerors who do not have electronic
capability to download the solicitation may submit a written request to
Maria Hernandez for a diskette copy of the solicitation. The requester
must include a self-addressed stamped envelope and an MS-DOS formatted
high-density 3 1/2" virus free diskette. Prospective offerors who fail
to submit an appropriate diskette or self-addressed stamped envelope
will not receive the solicitation. Pertinent information regarding this
solicitation can be found on the DOE Oakland Operations Office Home
Page. It is anticipated that the solicitation will be issued in May
1997. Although not a part of this solicitation, a NASA/JPL/DOE workshop
will be held on June 2-4, 1997 at the Doubletree Hotel in Pasadena,
California. The purpose of the workshop is to provide information on
NASA/JPL future plans for space exploration initiatives, progress in
small spacecraft technology and the need for improving radioisotope
power systems and the areas of improvement being sought. Additional
information on the workshop can be found on the DOE Oakland Operations
Office Home Page at http://www.oak.doe.gov. (0134) Loren Data Corp. http://www.ld.com (SYN# 0183 19970519\18-0001.SOL)
18 - Space Vehicles Index Page
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