[Federal Register: April 22, 2004 (Volume 69, Number 78)]
[Notices]
[Page 21867-21868]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr22ap04-92]
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
[Notice 04-053]
National Environmental Policy Act; Development of Advanced
Radioisotope Power Systems
AGENCY: National Aeronautics and Space Administration (NASA).
ACTION: Notice of intent to prepare a Tier I Environmental Impact
Statement (EIS) and to conduct scoping for the development of advanced
Radioisotope Power Systems.
SUMMARY: Pursuant to the National Environmental Policy Act of 1969
(NEPA), as amended (42 U.S.C. 4321 et seq.), the Council on
Environmental Quality Regulations for Implementing the Procedural
Provisions of NEPA (40 CFR parts 1500-1508), and NASA's policy and
procedures (14 CFR subpart 1216.3), NASA intends to conduct scoping and
to prepare a Tier I EIS for the development of advanced Radioisotope
Power Systems (RPSs). NASA, in cooperation with the U.S. Department of
Energy (DOE), proposes to develop in the near-term two types of
advanced RPSs to satisfy a wide of range of future space exploration
mission requirements. These advanced RPSs would both be capable of
functioning in the vacuum of space and in the environments encountered
on the surfaces of planets, moons and other solar system bodies. These
new power systems would be based upon a modified version of the General
Purpose Heat Source (GPHS) previously developed by DOE and used in the
Radioisotope Thermoelectric Generators (RTGs) for NASA's Galileo,
Ulysses, and Cassini missions. This modification would add additional
graphite material to the graphite aeroshell. The GPHS-based advanced
RPSs would be capable of providing long-term, reliable electrical power
to spacecraft across the range of conditions encountered in space and
planetary surface missions.
The Tier 1 EIS will also address in general terms the development
and qualification for flight of advanced RPSs that use passive or
dynamic systems to convert the heat generated from the decay of
plutonium to electrical energy, and related long-term research and
development of technologies that could further enhance the capability
of future RPS systems. The Multi-Mission Radioisotope Thermoelectric
Generator (MMRTG) and Stirling Radioisotope Generator (SRG) development
activity would include, but not necessarily be limited to: (1) New
power conversion technologies to more efficiently use the heat energy
from the GPHS module, and (2) improving the versatility of the RPS so
that it would be capable of operating for extended periods in the
vacuum of space and in planetary atmospheres. Specific future
developments of a new generation of space qualified RPSs (e.g., more
efficient systems than the proposed MMRTG or SRG, or systems with
smaller electrical power output) would be the subject of separate Tier
II environmental documentation.
DOE will be a cooperating agency in the preparation of this Tier 1
EIS.
DATES: Interested parties are invited to submit comments on
environmental concerns in writing on or before June 7, 2004, to assure
full consideration during the scoping process.
ADDRESSES: Comments should be addressed to Dr. George Schmidt, NASA
Headquarters, Code S, Washington, DC 20546-0001. While hardcopy
comments are preferred, comments may be sent by electronic mail to:
rpseis@nasa.gov.
FOR FURTHER INFORMATION CONTACT: Dr. George Schmidt, NASA Headquarters,
Code S, Washington, DC 20546-0001, by telephone at 202-358-0113, or by
electronic mail at rpseis@nasa.gov.
SUPPLEMENTARY INFORMATION: NASA's future scientific exploration of the
solar system is planned to include missions throughout the solar system
and potential missions to the surfaces of planets, moons and other
planetary bodies. Many of these missions cannot be accomplished with
current energy production and storage technologies available to NASA,
such as batteries, solar arrays, fuel cells, and the existing
radioisotope power system (the GPHS RTG). To enable this broad range of
missions, NASA is proposing to develop in the near-term, two types of
RPSs capable of functioning both in the vacuum of space and in the
environments encountered on the surfaces of planets, moons and other
planetary bodies.
NASA proposes to develop these advanced RPSs to enable missions
with substantial longevity, flexibility, and greater scientific
exploration capability. Some possibilities are:
- Comprehensive and detailed planetary investigations and creating comparative data sets of the outer planets--Jupiter, Saturn, Uranus, Neptune and Pluto and their moons. The knowledge gained with these data sets would be vital to understanding other recently discovered planetary systems and general principles of planetary formation.
- Comprehensive exploration of the surfaces and interiors of comets, possibly including returned samples to better understand the building blocks of our solar system and ingredients contributing to the origin of life.
- Expanded capabilities for surface and on-orbit exploration, and sample return missions to Mars and other planetary bodies (including the Earth's moon) to greatly improve our understanding of planetary processes, particularly those affecting the potential for life.
The current DOE radioisotope power system, the GPHS RTG, does not
meet these new or evolving mission requirements. The heat-to-
electricity converter for the existing RTG produces about 285 watts of
electrical power, but it is not designed to perform for an extended
period in planetary atmospheres such as that on Mars. The two new
proposed types of RPSs would be developed to meet the diverse needs of
future NASA space exploration missions.
Near-term advanced RPS development would focus on two power
systems, the MMRTG and the SRG. The MMRTG would build upon the
spaceflight-proven passive thermoelectric power conversion technology
incorporating improvements to allow extended operation in planetary
atmospheres. For the SRG, NASA would develop a new space-qualified
dynamic power conversion system, a Stirling engine, that would more
efficiently convert the heat from the decay of plutonium into electrical power and therefore use less
plutonium to generate comparable amounts of electrical power. Both of
these systems would provide up to about 100 watts of electric power and
would be capable of functioning both in the vacuum of space and in the
environments encountered on the surfaces of the planets, moons and
other bodies. Differences in SRG and MMRTG mechanical and thermal
interfaces would allow a broad range of mission specific spacecraft
designs. More than one MMRTG or SRG could be integrated with a
spacecraft to provide power levels exceeding 100 watts electrical.
This Tier I EIS will address in broad terms the technology
development activities of NASA, DOE, and the industrial contractors
involved in:
- Development and testing of advanced RPSs through final design, testing, and fabrication of flight qualified SRGs and MMRTGs, and
- Long-term research and development of technologies that could enhance the capabilities of future radioisotope power systems (e.g., systems that convert heat into electricity more efficiently and smaller systems).
It is anticipated that development and test activities involving
use of radioisotopes would be performed at existing DOE sites that
currently perform similar activities. Fuel processing and fabrication
would likely occur at existing facilities at Los Alamos National
Laboratory (LANL) in Los Alamos, New Mexico, which are currently used
for the fabrication of the fuel for the GPHS modules. Advanced RPS
assembly and testing would likely be performed at Argonne National
Laboratory--West (west of Idaho Falls, Idaho). These activities were
previously carried out at DOE's Mound, Ohio facility. Additional safety
testing of an integrated advanced RPS could be performed at one or more
of several existing facilities; including DOE facilities such as LANL
and Sandia National Laboratory (Albuquerque, New Mexico) or the U.S.
Army's Aberdeen Proving Grounds (Aberdeen, Maryland). Activities
associated with the development, testing, and verification of the power
conversion systems could be performed at several existing facilities
including some NASA facilities (Glenn Research Center at Lewis Field,
Cleveland, Ohio; and the Jet Propulsion Laboratory, Pasadena,
California) and several commercial facilities (Boeing Rocketdyne,
Canoga Park, California; Teledyne Energy Systems, Hunt Valley,
Maryland; Stirling Technology Corporation, Kennewick, Washington; and
Lockheed Martin, Valley Forge, Pennsylvania).
NASA plans to address the environmental impacts of the development
and use of Advanced RPSs through a two-tiered NEPA process. This Tier I
EIS will address the proposed development, overall purpose and need for
the development of advanced RPSs, development, testing and fabrication
of the MMRTG and SRG. This Tier 1 EIS will also address proposed
research and development work regarding technologies that could further
enhance the capabilities of future RPSs. Specific future developments
of a new generation of space qualified RPSs (e.g., more efficient
systems than the proposed MMRTG or SRG, or systems with smaller
electrical power output) would be the subject of separate Tier II
environmental documentation, as appropriate, using the most pertinent
data and analysis directly related to those developments. Mission-
specific use of any of these RPSs would be subject to separate
environmental documentation.
Alternatives to be considered in this Tier I EIS will include, but
will not necessarily be limited to the No Action Alternative, by which
NASA would not pursue development of advanced RPSs.
Written public input and comments on alternatives and environmental
impacts, and concerns associated with the development of advanced RPSs
are hereby requested.
Jeffrey E. Sutton,
Assistant Administrator for Institutional and Corporate Management.
[FR Doc. 04-9131 Filed 4-21-04; 8:45 am]
BILLING CODE 7510-01-P
