Associate Administrator for Commercial Space Transportation; Notice of availability and request for comment on a Draft Programmatic Environmental Impact Statement (PEIS) for Horizontal Launch and Reentry of Reentry Vehicles, 43930-43931 [05-14972]
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Federal Register / Vol. 70, No. 145 / Friday, July 29, 2005 / Notices
Elmhurst Public Library .................................................
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Glendale Heights Library ................................................
Glenview Public Library .................................................
Harold Washington Library ............................................
Hoffman Estates Library .................................................
Itasca Community Library ..............................................
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Melrose Park Public Library ...........................................
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Oakton Community College Library ..............................
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Written comments, faxes and e-mails
should be submitted to Michael W.
MacMullen of the FAA. The comment
period is open as of the date of this
Notice of Availability and closes at 5
p.m. central standard time, Tuesday,
September 6, 2005. The FAA will accept
comments on updated and/or refined
information in the following sections of
the FEIS and the associated appendices:
(1) Sections 3.6 and 3.7, of Chapter 3,
Alternatives.
(2) Sections 5.6, Air Quality, of
Chapter 5, Environmental
Consequences.
(3) Subsections 5.21.4 through
5.21.11, of Section 5.21, Environmental
Justice, of Chapter 5, Environmental
Consequences.
(4) Section 5.8, Section 4(f) and
Section 6(f) Resources, of Chapter 5,
Environmental Consequences.
(5) Section 5.22, Other Issues Relating
to Cemetery Acquisition, of Chapter 5,
Environmental Consequences.
(6) Section 5.23, Issues Relating to
Due Process Claims and Formal
Adjudicative Processes, of Chapter 5,
Environmental Consequences.
(7) Chapter 7, Mitigation.
Comments received via e-mail can
only be accepted with the full name and
address of the individual commenting.
FOR FURTHER INFORMATION CONTACT:
Michael W. MacMullen, Airports
Environmental Program Manager,
Federal Aviation Administration,
Chicago Airports District Office, 2300
East Devon Avenue, Des Plaines, IL
60018. Telephone: 847–294–8339, FAX:
847–294–7046, e-mail address:
ompeis@faa.gov.
VerDate jul<14>2003
17:05 Jul 28, 2005
Jkt 205001
211 Prospect Ave ............................................................
4 W Conti Pkwy ..............................................................
10311 Grand Ave ............................................................
25 E Fullerton Ave .........................................................
1930 Glenview Rd ..........................................................
400 S. State St .................................................................
1550 Hassell Rd ..............................................................
500 W. Irving Park Rd ....................................................
110 W Maple St ..............................................................
121 S. 5th Ave ................................................................
801 N. Broadway ............................................................
6140 Lincoln Ave ...........................................................
10 S Emerson St ..............................................................
6960 W Oakton St ...........................................................
231 N. Wolf Rd ...............................................................
834 Lake St ......................................................................
1616 E. Golf Rd ...............................................................
20 S Prospect Ave ...........................................................
735 Lathrop Ave .............................................................
8638 W. Grand Ave ........................................................
130 S Roselle Rd .............................................................
4200 Old River Rd ..........................................................
305 S Ardmore Ave ........................................................
520 N Wood Dale Rd ......................................................
Issued in Des Plaines, Illinois on July 20,
2005.
Barry Cooper,
Manager, Chicago Area Modernization
Program Office, Great Lakes Region.
[FR Doc. 05–14757 Filed 7–28–05; 8:45 am]
BILLING CODE 4910–13–M
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Associate Administrator for
Commercial Space Transportation;
Notice of availability and request for
comment on a Draft Programmatic
Environmental Impact Statement
(PEIS) for Horizontal Launch and
Reentry of Reentry Vehicles
Federal Aviation
Administration (FAA), Associate
Administrator for Commercial Space
Transportation (AST) is the lead Federal
agency for the development of this PEIS.
ACTION: Notice of Availability and
Request for Comment.
AGENCY:
SUMMARY: In accordance with National
Environmental Policy Act (NEPA)
regulations, the FAA is announcing the
availability of and requesting comments
on the Draft PEIS for Horizontal Launch
and Reentry of Reentry Vehicles. Under
the proposed action, the FAA would
license the launch of horizontally
launched vehicles and the reentry of
reentry vehicles (RVs). The FAA has
evaluated three horizontal launch
vehicle (LV) design concepts and both
powered and unpowered RV concepts.
This PEIS assesses the potential
programmatic environmental effects of
licensing horizontal launches and
reentries of RVs, as well as the licensing
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Fmt 4703
Sfmt 4703
Elmhurst.
Elmwood Park.
Franklin Park.
Glendale Heights.
Glenview.
Chicago.
Hoffman Estates.
Itasca.
Lombard.
Maywood.
Melrose Park.
Morton Grove.
Mount Prospect.
Niles.
Northlake.
Oak Park.
Des Plaines.
Park Ridge.
River Forest.
River Grove.
Schaumburg.
Schiller Park.
Villa Park.
Wood Dale.
of launch facilities that would support
horizontal launches and reentries. The
information in the PEIS is not intended
to address all site-specific launch issues.
This PEIS will be used to tier
subsequent environmental analyses for
site-specific launches, reentries, or the
operation of a launch or reentry site. To
facilitate these site-specific
environmental analyses the FAA has
provided guidance throughout the PEIS
in various sections and technical
appendices. This PEIS is intended to
update and replace the 1992 Final PEIS
for Commercial Reentry Vehicles and
complement the 2001 PEIS for Licensing
Launches.
DATES: The public comment period for
the NEPA process begins with the
publication of the U.S. Environmental
Protection Agency’s notice in the
Federal Register. To ensure that all
comments can be addressed in the Final
PEIS, comments must be received by the
FAA no later than September 12, 2005.
The FAA has developed a public
participation Web site (https://
ast.faa.gov/lrra/PEIS_Site.htm), where
the public can submit comments
electronically. Materials on the web site
include a downloadable electronic
version of the Draft PEIS; information
about licensing and the NEPA process;
frequently asked questions; and a public
comment form. Public hearings may be
requested by organizations or
individuals that feel their concerns
cannot be met through the available
opportunities to comment.
FOR FURTHER INFORMATION CONTACT:
Written and oral comments regarding
the Draft PEIS should be submitted to,
Mr. Doug Graham, FAA Environmental
Specialist, FAA PEIS, c/o ICF
Consulting, 9300 Lee Highway, Fairfax,
E:\FR\FM\29JYN1.SGM
29JYN1
Federal Register / Vol. 70, No. 145 / Friday, July 29, 2005 / Notices
VA 22031; e-mail
FAA.PEIS@icfconsulting.com; phone
(703) 934–3950; fax (703) 934–3951; or
through an online comment form
available at https://ast.faa.gov/lrra/
PEIS_info_resources.htm.
Additional Information: The proposed
action is for the FAA to issue licenses
for the launch of horizontally launched
vehicles and the reentry of RVs, as well
as the licensing of facilities that would
support horizontal launches and
reentries. The FAA exercises licensing
authority in accordance with the
Commercial Space Launch Act and
Commercial Space Transportation
Licensing Regulations, 14 CFR Ch. III,
which authorize the FAA to license the
launch of an LV or the reentry of an RV
when conducted within the U.S. and
those operated by U.S. citizens abroad.
The scope of the PEIS includes launches
on orbital and suborbital trajectories
from both existing government launch
facilities and nonfederal launch sites in
the U.S. and abroad.
The FAA identified three types of
LVs, called out in this analysis as
Concept 1, Concept 2, and Concept 3,
which would be typical of the vehicles
that would operate within the activities
specified in this PEIS. Additionally,
both powered and unpowered RV
concepts are considered in this analysis.
This PEIS may be used to tier
subsequent environmental
documentation that the FAA would use
to make a determination about licensing
the launches and reentries of the
aforementioned types of LVs and RVs.
Additional environmental analysis
would need to be conducted for any
activity that is not addressed in this
Draft PEIS or in previous environmental
analyses.
Launch vehicles included in Concept
1 would use jet-powered take off with
subsequent rocket ignition, and conduct
a powered horizontal landing. These
LVs would take off from conventional
runways using jet power, and then
ignite rocket engines at a specified
altitude. The LV would use either
suborbital or orbital trajectories
depending on the mission. During
descent, jet engines would be restarted
at a specified altitude and the vehicle
would fly to a powered, horizontal
landing at a designated location.
Launch vehicles included in Concept
2 would use rocket powered take off and
flight, and a non-powered horizontal
landing. The rocket motors would be
ignited while the LV is on the runway.
After takeoff, the LV would follow a
steep ascent trajectory that could be
suborbital or orbital. The vehicle would
not use powered descent but would
VerDate jul<14>2003
17:05 Jul 28, 2005
Jkt 205001
glide to a horizontal landing at a
designated location.
Launch vehicles included in Concept
3 would be carried aloft via assist
aircraft with subsequent rocket ignition,
and would conduct a non-powered
horizontal landing. The vehicle would
be comprised of an assist aircraft, such
as a carrier or tow aircraft, and an LV,
which would range from 9 to 46 meters
(30 to 150 feet) in length. Depending on
the design configuration, the LV could
be attached to the top, mated to the
underside, or tethered to the assist
aircraft. After taking off on a horizontal
runway, the LV would be released from
the assist aircraft and rocket engines on
the LV would be fired. The assist
aircraft would make a powered
horizontal landing after releasing the
LV. The LV trajectory could be either
orbital or suborbital. The LV would not
use powered descent but would glide to
a horizontal landing at a designated
location.
Reentry vehicle concepts include both
unpowered and powered vehicles. Once
an unpowered RV concept enters Earth’s
atmosphere, it would glide, deploy a
parachute or parafoil, and descend to
the Earth’s surface. Once a powered RV
concept enters Earth’s atmosphere, a
propulsion system would be used to
control descent and direct the RV to a
landing site. Both RV concepts could be
oriented vertically or horizontally
during reentry and subsequent landing.
The design and size of the RV dictates
whether descent would be powered or
unpowered. Some RVs would descend
using a combination of unpowered and
powered methods. For example, a rocket
engine would be fired to slow initial
descent, then a parachute would be
deployed and finally when the RV is
close to Earth’s surface rocket engines
would be fired for a final touch down.
Three alternatives to the proposed
action were considered in the Draft
PEIS. The first alternative would be to
issue licenses for orbital Reusable
Launch Vehicles (RLVs) using
unpowered reentry and landing only.
The second alternative would be to
issue licenses to orbital RLVs using
powered reentry and landing only. The
third alternative would be to issue
licenses of horizontal launches of RLVs
where full rocket engine ignition occurs
at or above 914 meters (3,000 feet).
Under the No Action Alternative, the
FAA would not issue licenses for the
horizontal launch of LVs and reentry of
RVs, as well as the operation of launch
and reentry sites for such activities.
Potential impacts of the proposed
action and alternatives were analyzed in
the Draft PEIS. Potential environmental
impacts of successful launches include
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Frm 00095
Fmt 4703
Sfmt 4703
43931
impacts to the atmosphere, airspace,
biological resources, cultural resources,
public health and safety, hazardous
materials and hazardous waste, geology
and soils, land use, noise,
socioeconomics, environmental justice,
section 4(f) resources, orbital debris,
aesthetic and visual resources, and
water resources. The impacts of the No
Action Alternative would be the same as
those described for the affected
environment in the Draft PEIS.
Potential cumulative impacts of the
proposed action are also addressed in
the Draft PEIS.
Dated: July 20, 2005.
John Sloan,
Acting Manager, Space Systems Development
Division.
[FR Doc. 05–14972 Filed 7–28–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Maritime Administration
[Docket Number 2005–21918]
Requested Administrative Waiver of
the Coastwise Trade Laws
Maritime Administration,
Department of Transportation.
ACTION: Invitation for public comments
on a requested administrative waiver of
the Coastwise Trade Laws for the vessel
Avocation.
AGENCY:
SUMMARY: As authorized by Pub. L. 105–
383 and Pub. L. 107–295, the Secretary
of Transportation, as represented by the
Maritime Administration (MARAD), is
authorized to grant waivers of the U.S.build requirement of the coastwise laws
under certain circumstances. A request
for such a waiver has been received by
MARAD. The vessel, and a brief
description of the proposed service, is
listed below. The complete application
is given in DOT docket 2005–21918 at
https://dms.dot.gov. Interested parties
may comment on the effect this action
may have on U.S. vessel builders or
businesses in the U.S. that use U.S.-flag
vessels. If MARAD determines, in
accordance with Pub. L. 105–383 and
MARAD’s regulations at 46 CFR part
388 (68 FR 23084; April 30, 2003), that
the issuance of the waiver will have an
unduly adverse effect on a U.S.-vessel
builder or a business that uses U.S.-flag
vessels in that business, a waiver will
not be granted. Comments should refer
to the docket number of this notice and
the vessel name in order for MARAD to
properly consider the comments.
Comments should also state the
commenter’s interest in the waiver
application, and address the waiver
E:\FR\FM\29JYN1.SGM
29JYN1
Agencies
[Federal Register Volume 70, Number 145 (Friday, July 29, 2005)]
[Notices]
[Pages 43930-43931]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-14972]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Associate Administrator for Commercial Space Transportation;
Notice of availability and request for comment on a Draft Programmatic
Environmental Impact Statement (PEIS) for Horizontal Launch and Reentry
of Reentry Vehicles
AGENCY: Federal Aviation Administration (FAA), Associate Administrator
for Commercial Space Transportation (AST) is the lead Federal agency
for the development of this PEIS.
ACTION: Notice of Availability and Request for Comment.
-----------------------------------------------------------------------
SUMMARY: In accordance with National Environmental Policy Act (NEPA)
regulations, the FAA is announcing the availability of and requesting
comments on the Draft PEIS for Horizontal Launch and Reentry of Reentry
Vehicles. Under the proposed action, the FAA would license the launch
of horizontally launched vehicles and the reentry of reentry vehicles
(RVs). The FAA has evaluated three horizontal launch vehicle (LV)
design concepts and both powered and unpowered RV concepts. This PEIS
assesses the potential programmatic environmental effects of licensing
horizontal launches and reentries of RVs, as well as the licensing of
launch facilities that would support horizontal launches and reentries.
The information in the PEIS is not intended to address all site-
specific launch issues. This PEIS will be used to tier subsequent
environmental analyses for site-specific launches, reentries, or the
operation of a launch or reentry site. To facilitate these site-
specific environmental analyses the FAA has provided guidance
throughout the PEIS in various sections and technical appendices. This
PEIS is intended to update and replace the 1992 Final PEIS for
Commercial Reentry Vehicles and complement the 2001 PEIS for Licensing
Launches.
DATES: The public comment period for the NEPA process begins with the
publication of the U.S. Environmental Protection Agency's notice in the
Federal Register. To ensure that all comments can be addressed in the
Final PEIS, comments must be received by the FAA no later than
September 12, 2005. The FAA has developed a public participation Web
site (https://ast.faa.gov/lrra/PEIS_Site.htm), where the public can
submit comments electronically. Materials on the web site include a
downloadable electronic version of the Draft PEIS; information about
licensing and the NEPA process; frequently asked questions; and a
public comment form. Public hearings may be requested by organizations
or individuals that feel their concerns cannot be met through the
available opportunities to comment.
FOR FURTHER INFORMATION CONTACT: Written and oral comments regarding
the Draft PEIS should be submitted to, Mr. Doug Graham, FAA
Environmental Specialist, FAA PEIS, c/o ICF Consulting, 9300 Lee
Highway, Fairfax,
[[Page 43931]]
VA 22031; e-mail FAA.PEIS@icfconsulting.com; phone (703) 934-3950; fax
(703) 934-3951; or through an online comment form available at https://
ast.faa.gov/lrra/PEIS_info_resources.htm.
Additional Information: The proposed action is for the FAA to issue
licenses for the launch of horizontally launched vehicles and the
reentry of RVs, as well as the licensing of facilities that would
support horizontal launches and reentries. The FAA exercises licensing
authority in accordance with the Commercial Space Launch Act and
Commercial Space Transportation Licensing Regulations, 14 CFR Ch. III,
which authorize the FAA to license the launch of an LV or the reentry
of an RV when conducted within the U.S. and those operated by U.S.
citizens abroad. The scope of the PEIS includes launches on orbital and
suborbital trajectories from both existing government launch facilities
and nonfederal launch sites in the U.S. and abroad.
The FAA identified three types of LVs, called out in this analysis
as Concept 1, Concept 2, and Concept 3, which would be typical of the
vehicles that would operate within the activities specified in this
PEIS. Additionally, both powered and unpowered RV concepts are
considered in this analysis. This PEIS may be used to tier subsequent
environmental documentation that the FAA would use to make a
determination about licensing the launches and reentries of the
aforementioned types of LVs and RVs. Additional environmental analysis
would need to be conducted for any activity that is not addressed in
this Draft PEIS or in previous environmental analyses.
Launch vehicles included in Concept 1 would use jet-powered take
off with subsequent rocket ignition, and conduct a powered horizontal
landing. These LVs would take off from conventional runways using jet
power, and then ignite rocket engines at a specified altitude. The LV
would use either suborbital or orbital trajectories depending on the
mission. During descent, jet engines would be restarted at a specified
altitude and the vehicle would fly to a powered, horizontal landing at
a designated location.
Launch vehicles included in Concept 2 would use rocket powered take
off and flight, and a non-powered horizontal landing. The rocket motors
would be ignited while the LV is on the runway. After takeoff, the LV
would follow a steep ascent trajectory that could be suborbital or
orbital. The vehicle would not use powered descent but would glide to a
horizontal landing at a designated location.
Launch vehicles included in Concept 3 would be carried aloft via
assist aircraft with subsequent rocket ignition, and would conduct a
non-powered horizontal landing. The vehicle would be comprised of an
assist aircraft, such as a carrier or tow aircraft, and an LV, which
would range from 9 to 46 meters (30 to 150 feet) in length. Depending
on the design configuration, the LV could be attached to the top, mated
to the underside, or tethered to the assist aircraft. After taking off
on a horizontal runway, the LV would be released from the assist
aircraft and rocket engines on the LV would be fired. The assist
aircraft would make a powered horizontal landing after releasing the
LV. The LV trajectory could be either orbital or suborbital. The LV
would not use powered descent but would glide to a horizontal landing
at a designated location.
Reentry vehicle concepts include both unpowered and powered
vehicles. Once an unpowered RV concept enters Earth's atmosphere, it
would glide, deploy a parachute or parafoil, and descend to the Earth's
surface. Once a powered RV concept enters Earth's atmosphere, a
propulsion system would be used to control descent and direct the RV to
a landing site. Both RV concepts could be oriented vertically or
horizontally during reentry and subsequent landing. The design and size
of the RV dictates whether descent would be powered or unpowered. Some
RVs would descend using a combination of unpowered and powered methods.
For example, a rocket engine would be fired to slow initial descent,
then a parachute would be deployed and finally when the RV is close to
Earth's surface rocket engines would be fired for a final touch down.
Three alternatives to the proposed action were considered in the
Draft PEIS. The first alternative would be to issue licenses for
orbital Reusable Launch Vehicles (RLVs) using unpowered reentry and
landing only. The second alternative would be to issue licenses to
orbital RLVs using powered reentry and landing only. The third
alternative would be to issue licenses of horizontal launches of RLVs
where full rocket engine ignition occurs at or above 914 meters (3,000
feet). Under the No Action Alternative, the FAA would not issue
licenses for the horizontal launch of LVs and reentry of RVs, as well
as the operation of launch and reentry sites for such activities.
Potential impacts of the proposed action and alternatives were
analyzed in the Draft PEIS. Potential environmental impacts of
successful launches include impacts to the atmosphere, airspace,
biological resources, cultural resources, public health and safety,
hazardous materials and hazardous waste, geology and soils, land use,
noise, socioeconomics, environmental justice, section 4(f) resources,
orbital debris, aesthetic and visual resources, and water resources.
The impacts of the No Action Alternative would be the same as those
described for the affected environment in the Draft PEIS.
Potential cumulative impacts of the proposed action are also
addressed in the Draft PEIS.
Dated: July 20, 2005.
John Sloan,
Acting Manager, Space Systems Development Division.
[FR Doc. 05-14972 Filed 7-28-05; 8:45 am]
BILLING CODE 4910-13-P