Office of Commercial Space Transportation; Waiver of Autonomous Reentry Restriction for a Reentry Vehicle, 75621-75624 [2010-30399]
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Federal Register / Vol. 75, No. 233 / Monday, December 6, 2010 / Rules and Regulations
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ii. Consistency With Rationale for
Section 431.35
iii. Other Factors Impacting the Waiver
Decision
The next matter that the FAA
addressed was whether granting a
waiver in this case would be consistent
with the safety rationale underlying
section 431.35. In the preamble to the
notice of proposed rulemaking (NPRM),
the FAA explained that, when it was
drafting section 431.35, it decided to use
a single aggregate risk threshold for a
mission involving the launch and
reentry of a reentry vehicle. Commercial
Space Transportation Reusable Launch
Vehicle and Reentry Licensing
Regulations, NPRM, 64 FR 19626, 19635
(Apr. 21, 1999). However, the FAA also
acknowledged that there could be
circumstances where it would be
appropriate to separate launch from
reentry risk, such as where different
operators were involved and could be
apportioned allowable risk thresholds,
or where intervening events or time
made reentry risks sufficiently
independent of launch risks as to
warrant separate consideration. Id.
Here, the health check of Dragon, a
different vehicle than the Falcon 9
launch vehicle, that will take place once
Dragon is in orbit is an intervening
event that makes the launch risk
associated with the launch of Falcon 9
independent of the reentry risk
associated with the reentry of Dragon.
The health check will permit SpaceX to
reevaluate Dragon’s condition after the
launch has taken place, and to make a
fresh determination about whether
Dragon should be permitted to reenter.
If, after conducting a post-launch health
check of Dragon, SpaceX finds safety
concerns associated with reentry,
SpaceX will be able to issue a command
to disable Dragon’s reentry. As such,
because the reentry of Dragon is based
on the results of an in-orbit health check
that will be conducted independently of
the launch, the risks associated with the
launch of Falcon 9 and reentry of
Dragon are sufficiently independent to
warrant separate consideration in this
case.
Evaluating these risks separately, the
Ec for the launch of Falcon 9 is 19 ×
10¥6, which is within the 30 × 10¥6
limit imposed by section 431.35(b)(1)(i).
Likewise, the Ec for the reentry of
Dragon is 28 × 10¥6, which is also
within the 30 × 10¥6 limit that the FAA
applies to launch hazards. Accordingly,
the FAA has determined that granting a
waiver in this case would be consistent
with the safety rationale underlying
section 431.35.
Dragon’s mitigation measures were
another factor that influenced the FAA’s
analysis with regard to whether a waiver
would jeopardize public health and
safety and safety of property. As stated
above, the Dragon capsule employs
numerous risk mitigation measures to
reduce the risk to the public from the
launch of Falcon 9 and reentry of
Dragon.
The FAA has taken particular notice
of the way in which Dragon’s electrical
power system (batteries), flight
computer, and propulsion system will
reduce risk to the public. For instance,
Dragon has more than four times the
propellant needed for a safe reentry in
the target area. The additional
propellant increases the probability that
Dragon will land in its nominal target
area instead of a population center.
Dragon also has three parachutes, which
decrease risk to the public because only
one of these parachutes is necessary for
a low impact landing. The additional
parachutes reduce the chance that
Dragon will crash into the ground while
attempting to land.
SpaceX has also designed the Dragon
reentry vehicle to vent propellants in
the case of an aborted or off-nominal
reentry. This mitigation measure greatly
reduces the risk to the public because it
allows Dragon to safely dispose of
hazardous propellant materials if
something should go wrong with the
mission.
As a result of Dragon’s mitigation
measures, as well as the other
considerations discussed above, the
FAA has determined that granting a
waiver in this case would not jeopardize
public health and safety or safety of
property.
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B. National Security and Foreign Policy
Implications
The FAA has identified no national
security or foreign policy implications
associated with granting this waiver.
C. Public Interest
Two of the public policy goals of
Chapter 701 are: (1) To promote
economic growth and entrepreneurial
activity through use of the space
environment; and (2) to encourage the
United States private sector to provide
launch and reentry vehicles and
associated services. 49 U.S.C.
70101(b)(1) and (2). Here, granting this
waiver is consistent with the public
interest goals articulated by Chapter
701.
A goal of the COTS program’s mission
is to ultimately develop the capability to
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75621
resupply the International Space
Station. SpaceX’s demonstration launch
of Falcon 9 and reentry of Dragon is a
step toward achieving that goal. This
demonstration launch is important in
light of the fact that the U.S.
Government is ending the Space Shuttle
Program and NASA plans to rely upon
its COTS Program to develop a robust
domestic commercial space
transportation capability. This
capability will provide the United States
with the ability to resupply the
International Space Station. As such,
granting SpaceX’s waiver request will be
consistent with Chapter 701’s policy
goals by: (1) Promoting SpaceX’s
entrepreneurial activity in the space
environment; and (2) encouraging a
private U.S. company to develop and
launch a launch vehicle (Falcon 9) and
a reentry vehicle (Dragon).
Summary and Conclusion
A waiver will not jeopardize public
health and safety or safety of property
because: (1) The risk associated with the
launch of Falcon 9 and the risk
associated with the reentry of Dragon
are each under an Ec of 30 × 10¥6; and
(2) the Dragon capsule employs
numerous risk mitigation measures
including an in-orbit health check. The
waiver also will not jeopardize national
security and foreign policy interests of
the United States. A waiver is in the
public interest because it furthers the
statutory goals of Chapter 701. For the
foregoing reasons, the FAA has waived
the restriction that the combined risk to
the public from the launch of Falcon 9
and reentry of Dragon cannot exceed an
expected average number of 0.00003
casualties (30 × 10¥6) from debris.
Issued in Washington, DC, on November
30, 2010.
Kenneth Wong,
Commercial Space Transportation, Licensing
and Safety Division Manager.
[FR Doc. 2010–30402 Filed 12–3–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 431
Office of Commercial Space
Transportation; Waiver of Autonomous
Reentry Restriction for a Reentry
Vehicle
Federal Aviation
Administration (FAA), DOT.
AGENCY:
ACTION:
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Notice of waiver.
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Federal Register / Vol. 75, No. 233 / Monday, December 6, 2010 / Rules and Regulations
This notice of waiver
concerns two petitions for waiver
submitted to the Federal Aviation
Administration (FAA) by Space
Exploration Technologies Corp.
(SpaceX): A petition to waive the
requirement that a waiver petition be
submitted at least sixty days before the
proposed effective date of the waiver,
and a petition to waive the requirement
that SpaceX only initiate reentry of its
reentry vehicle, the Dragon Spacecraft
(Dragon), by command. The first
petition is unnecessary because, as
explained below, SpaceX demonstrated
good cause for its late filing. The FAA
finds that waiving the requirement for
SpaceX ground operators to initiate
Dragon’s reentry to Earth is in the public
interest and will not jeopardize public
health and safety, safety of property,
and national security and foreign policy
interests of the United States.
FOR FURTHER INFORMATION CONTACT: For
technical questions concerning this
waiver contact Howard Searight,
Aerospace Engineer, AST–200, Office of
Commercial Space Transportation
(AST), Federal Aviation Administration,
800 Independence Avenue, SW.,
Washington, DC 20591; telephone (202)
267–7927; e-mail:
howard.searight@faa.gov. For legal
questions concerning this waiver
contact Laura Montgomery, Senior
Attorney for Commercial Space
Transportation, AGC–200, Office of the
Chief Counsel, Regulations Division,
Federal Aviation Administration, 800
Independence Avenue, SW.,
Washington, DC 20591; telephone (202)
267–3150; e-mail:
laura.montgomery@faa.gov.
SUPPLEMENTARY INFORMATION:
Background: On September 23, 2010,
SpaceX requested two waivers from the
FAA’s Office of Commercial Space
Transportation (AST) for the reentry of
Dragon, a reentry vehicle, to be
launched on Falcon 9 flight 002. First,
SpaceX requested a waiver of
procedural requirements for waivers set
forth at 14 CFR 404.3. Second, SpaceX
requested a waiver of 14 CFR 431.43(e)1
to allow autonomous reentry.2
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SUMMARY:
1 Even though Dragon is a reentry vehicle and not
a reusable launch vehicle, 14 CFR 435.33
incorporates and applies section 431.43 to all
reentry vehicles.
2 SpaceX stated that autonomous reentry would
only be used in off-nominal circumstances, and the
regulation prevents autonomous reentry only for
nominal circumstances, thus rendering a waiver
unnecessary. This interpretation of the regulation
conflicts with the regulation’s requirement that an
operator only initiate reentry by command as
described in the preamble to the proposed rule.
There, the FAA expressed its concern that
authorizing reentry of totally autonomous vehicles
would not fulfill adequately its public safety
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The FAA licenses, in relevant part,
the launch of a launch vehicle, and
reentry of a reentry vehicle under
authority granted to the Secretary of
Transportation by 49 U.S.C. Subtitle IX,
chapter 701 (Chapter 701), and
delegated to the FAA’s Administrator
and Associate Administrator for
Commercial Space Transportation.
SpaceX is a private commercial space
flight company. It entered into a Space
Act Agreement with the National
Aeronautics and Space Administration
(NASA) as part of NASA’s Commercial
Orbital Transportation Services (COTS)
program. The COTS program is
designed to stimulate efforts within the
private sector to demonstrate safe,
reliable, and cost-effective space
transportation to the International Space
Station.
SpaceX’s petition for waiver concerns
an upcoming demonstration flight that it
plans to undertake as part of the COTS
program. At the time of the filing of the
petition, the launch for that flight was
scheduled to take place on November 8,
2010. During the flight, SpaceX’s Falcon
9 vehicle will launch the Dragon reentry
vehicle into orbit. Dragon is a reentry
vehicle whose capability SpaceX plans
to demonstrate for NASA. Ultimately,
SpaceX intends to use Dragon to
transport cargo and people to and from
the International Space Station.
Once Dragon is in orbit, a groundimplemented health check will be
carried out by telemetry. SpaceX has
designed the Dragon capsule to remain
in orbit until SpaceX ground operators
transmit a reentry command. A ground
operator can issue commands to either
enable or disable the reentry of Dragon
based on the health of the vehicle.
Dragon is also able to conduct an
autonomous health check. Propellant
and power levels are the key variables
used by ground operators in
determining whether to issue
commands to reenter or stay in orbit,
and the same variables would be used
by the vehicle in its onboard health
check. The onboard health check is
designed to check time-dependent
variables to ensure the health and
functionality of the propellant, power
and avionics sub-systems. Based on
these evaluations, Dragon is able to
determine whether it is healthy. On the
ground, the reentry team can read the
responsibility. Without active control, those
systems and conditions necessary for safe reentry
would not be verified before reentry was initiated
Commercial Space Transportation Reusable Launch
Vehicle and Reentry Licensing Regulations, 64 FR
19626, 19645 (Apr. 21, 1999) (Reentry NPRM).
Because it was the FAA’s intent that the regulations
ensure human control capability upon reentry,
SpaceX’s petition is a request for a waiver.
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raw data and establish for themselves
whether Dragon is healthy. Dragon’s
onboard health check is designed to
replicate the decision-making process of
the ground operators with respect to
time-dependent failures, which are, in
Dragon’s case, the full depletion of
power and propellant. If Dragon’s
communications failed and the vehicle
passed the onboard health check,
Dragon would reenter autonomously.
Once Dragon passes a groundimplemented health check, ground
operators will issue a reentry command.
After ground operators issue the reentry
command, Dragon will wait until the
point in space at which the reentry burn
initiation is planned before initiating
reentry. Dragon will reenter, deploy
three parachutes and splash down. A
nominal Dragon reentry splashes down
in the Pacific Ocean off the coast of
southern California with some
propellants on board.
If an anomaly occurs after the
issuance of the reentry command,
ground operators can issue a command
that disables reentry. SpaceX is
concerned with what would happen if
its ground operators were unable to
communicate a reentry command to a
healthy Dragon due to failed or disabled
communications. In this circumstance,
SpaceX proposes that the FAA permit
the autonomous reentry of a healthy
Dragon at the nominal landing location
in order to maximize public safety. This
scenario may play out in different ways.
If ground operators needed more time to
complete a health check than that
available during one orbit, they could
disable reentry by command. Dragon
would then not reenter, even if its
autonomous health check would
otherwise allow it to. If a health check
proved satisfactory, ground operators
could re-enable reentry, and Dragon
would reenter. If Dragon never received
a command, it could rely on the results
of its own continuous autonomous
health check, and, if those results were
positive, reenter.
Dragon has several safety features that
would allow for a safe autonomous
reentry in the event of a
communications failure, including:
(1) The vehicle automatically reduces
itself to its lowest energy level in the
case of an off-nominal burn; (2) the
vehicle has the ability to autonomously
guide itself to the same pre-determined
landing site, located more than 780
kilometers from the coastline; (3) the
vehicle has the ability to monitor its
safety-critical systems in real-time; (4)
the vehicle has over 100% margin on
both power and propellant budgets; (5)
the vehicle has a space-grade inertial
measurement unit (IMU); (6) the vehicle
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Federal Register / Vol. 75, No. 233 / Monday, December 6, 2010 / Rules and Regulations
has a space-grade flight computer; and
(7) the vehicle has redundant drogue
parachutes and dual redundant main
parachutes.
Waiver Criteria: Chapter 701 allows
the FAA to waive a requirement for an
individual license applicant if the FAA
decides that the waiver will not
jeopardize public health and safety,
safety of property, and national security
and foreign policy interests of the
United States and is in the public
interest. 49 U.S.C. 70105(b)(3) (2010);
14 CFR 404.5(b) (2010).
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Section 404.3 Waiver Petition
Section 404.3(b)(5) requires that a
petition for waiver be submitted at least
sixty days before the proposed effective
date of the waiver. However, this
section also provides that a petition may
be submitted late if the petitioner shows
good cause. Id. (b)(5).
Here, SpaceX submitted its waiver
petition on September 23, 2010, which
was less than sixty days before the
November 8, 2010 launch date planned
at the time of the filing of the petition.
However, in its petition, SpaceX
explained that it initially interpreted the
applicable regulations differently than
the FAA, and was not aware that a
waiver would be required. Once the
FAA informed SpaceX that it needed to
obtain a waiver, SpaceX proceeded to
apply for the waiver in a timely fashion.
As such, the FAA has found that
SpaceX had good cause for submitting
its waiver petition less than sixty days
from its launch date. Therefore,
SpaceX’s late submission does not
violate 404.3(b)(5), and a waiver of that
section is unnecessary.
Section 431.43(e) Waiver Petition
Section 431.43(e) requires, in
pertinent part, any operator of a
reusable launch vehicle that enters
Earth orbit to issue a command enabling
reentry flight of the vehicle. It further
states that reentry flight cannot be
initiated autonomously under nominal
circumstances without prior enable.
14 CFR 431.43(e).
For reasons described below, the FAA
waives the requirement of 14 CFR
431.43(e), and allows SpaceX to
autonomously initiate reentry flight of
Dragon in the event that SpaceX ground
operators lose communication with
Dragon, and Dragon is healthy. In this
context, communication loss means
Dragon fails to send a reentry request to
SpaceX’s ground operators, or the
ground operators are unable to send a
command enabling reentry of Dragon.
The onboard health check is designed to
check time-dependent variables to
ensure the health and functionality of
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the propellant, power and avionics subsystems.
In deciding whether or not to waive
the requirement that Dragon’s operator
issue a command to enable reentry of
the vehicle, the FAA must analyze
whether the waiver: (1) Is in the public
interest; (2) will not jeopardize public
health and safety or safety of property;
and (3) will not jeopardize national
security and foreign policy interests of
the United States. 49 U.S.C. 70105(b)(3);
14 CFR 404.5(b). The FAA will grant
this waiver because SpaceX satisfies the
criteria.
A. Public Interest
The change proposed by SpaceX is
consistent with the statutory goal of
seeking improvements to safety. 49
U.S.C. 70101(a)(12) and (b)(2)(C).
Granting SpaceX’s waiver is in the
public interest because a guided reentry
is safer than a random reentry, and
therefore Dragon’s proposed
autonomous reentry capability enhances
the overall safety of the mission.
B. Public Health and Safety
Although the FAA’s regulation
prohibits autonomous reentry, a waiver
is warranted in SpaceX’s case because
an autonomous reentry of a healthy
Dragon that has lost ground
communications is safer than a random
reentry. The preamble to the Reentry
NPRM acknowledges that some RLV
operators were contemplating totally
autonomous reentry capability, and
expressed a concern that autonomous
reentry was not adequately safe.
Specifically, the FAA was concerned
about system anomalies or other noncompliant conditions that would not be
verified before initiation of reentry in
the absence of active human control.
Reentry NPRM, 64 FR at 19645. The
FAA retained flexibility in granting
waivers to allow the use of autonomous
systems. Commercial Space
Transportation Reusable Launch
Vehicle and Reentry Licensing
Regulations, 65 FR 56618, 56641 (Sept.
19, 2000) (Reentry Rule). In requiring
the capability for human intervention,
the FAA did not intend to foreclose the
use of autonomous systems or
autonomous decision-making. Id.
SpaceX’s proposed approach addresses
the concern underlying the regulatory
requirements and poses less risk than
that associated with Dragon being left in
orbit to reenter randomly at some later
time. SpaceX’s mitigation measures are
of additional importance to the FAA’s
decision to grant a waiver.
The FAA’s reason for requiring
commanded reentry was to make sure
that an operator had the chance to verify
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75623
that there were no system anomalies or
other non-compliant conditions. Under
SpaceX’s proposed plan, the operator
would employ two means of detecting
any such anomalies. Ground operators
and Dragon’s own continuous
autonomous health check would both
perform health checks to determine
whether conditions prohibited reentry.
To determine the effect of granting
SpaceX’s waiver on public safety, the
FAA performed a risk analysis of
potential reentry outcomes. The risks of
leaving the vehicle in orbit or
attempting a reentry (whether
autonomous or commanded) are best
compared by applying conditional
probabilities, where an undesired event
is assumed to happen, to each
possibility. For purposes of comparison,
in the two cases discussed below, the
FAA assumes that Dragon fails to expel
its propellant, and its parachutes fail to
deploy, resulting in an explosive
impact.
In a random reentry scenario, Dragon
has lost communications and is unable
to reenter autonomously. The FAA
assumed a 100% probability of leaving
the vehicle in orbit with a full
propellant load. The vehicle would
continue circling the Earth until it
reentered randomly due to natural
orbital decay. The FAA assumed the
impact probability in a given latitude
band was equivalent to the dwell time
of the vehicle in orbit over that latitude
band. The FAA computed the
population density as a function of
latitude by dividing the population
within each latitude band under Dragon
by the Earth’s surface area within each
latitude band. The FAA applied a
sheltering model based on surveys and
socioeconomic factors, including
population density and distribution and
the types of homes people live in, all of
which affect expected casualties. The
conditional risk computed for a random
reentry produced an expected average
number of casualties (Ec) of
approximately 23 × 10¥3.
In an autonomous reentry scenario,
Dragon has lost communications and is
attempting an autonomous reentry. The
FAA assumed a 100% probability of
reentry burn failure at any time from
burn initiation to burn cutoff, assuming
a uniform failure rate. In this scenario,
Dragon remains orbital for two-thirds of
its burn. Two-thirds of the conditional
random reentry risk calculated above
results in an Ec of approximately 15 ×
10¥3. The remaining risk results from
an assumed failure during the last third
of the reentry burn when the vehicle is
no longer in orbit. This results in a flight
corridor extending from the Atlantic to
the Pacific crossing over the continental
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Federal Register / Vol. 75, No. 233 / Monday, December 6, 2010 / Rules and Regulations
jdjones on DSK8KYBLC1PROD with RULES
United States and Northern Mexico. The
conditional risk along this flight
corridor is approximately Ec 13 × 10¥3.
The FAA multiplied 13 × 10¥3 by onethird, to account for the fact that this
failure mode is only applicable to onethird of the burn, which results in an Ec
of 41 × 10¥4. The total conditional risk
associated with an autonomous reentry,
where a burn failure is assumed, is 19
× 10¥3. Thus, there is theoretically 20%
less risk in an attempt to reenter Dragon
than there is in leaving it in orbit given
a communications failure.
Also of importance to the FAA’s
decision to grant a waiver, Dragon is
equipped with a number of mitigating
features. First, the vehicle automatically
safes itself in the case of an off-nominal
burn. This means that if Dragon
conducted its reentry burn, but
computed that the desired landing spot
would not be achieved, it would vent
the rest of its fuel, thereby reducing the
possibility of explosion or dispersion of
toxic fumes on impact. Second, the
vehicle has the ability to autonomously
guide itself to its planned landing
location in the Pacific Ocean, some 780
kilometers from the coastline. This
internal capability allows Dragon to act
independently, based on programmed
instructions and information regarding
its location, if communications with the
ground are lost. Third, the vehicle has
the ability to monitor its safety-critical
systems in real-time. This means Dragon
has near-immediate awareness of the
operability of its on-board systems that
allow it to operate safely, and this
awareness enables Dragon to react in
time to conduct a reentry. Fourth, the
vehicle has a space-grade IMU and flight
computer. This means Dragon is
equipped with a system that provides
information on where Dragon is, which
is pertinent to its guidance capabilities,
and the IMU and flight computer are
designed and tested to operate in the
rigorous conditions of space.
the foregoing reasons, the FAA has
waived the requirement of 14 CFR
431.43(e) for a commanded reentry, and
allows SpaceX to autonomously initiate
reentry flight of Dragon in the event that
all communication between ground
operators and Dragon has been lost, and
Dragon is healthy.
C. National Security and Foreign Policy
Implications
The FAA has not identified any
national security or foreign policy
implications associated with granting
this waiver.
Summary and Conclusion: A waiver
is in the public interest because it
accomplishes the goals of Chapter 701
and decreases risk to the public. The
waiver will not jeopardize public health
and safety or safety of property because
allowing autonomous reentry of a
healthy Dragon vehicle that has lost all
communications presents less risk than
a random reentry. A waiver will not
jeopardize national security and foreign
policy interests of the United States. For
SUPPLEMENTARY INFORMATION:
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Issued in Washington, DC on November 30,
2010.
Kenneth Wong,
Licensing and Safety Division Manager.
[FR Doc. 2010–30399 Filed 12–3–10; 8:45 am]
BILLING CODE 4910–13–P
LIBRARY OF CONGRESS
Copyright Royalty Board
37 CFR Part 386
[Docket No. 2010–10 CRB Satellite COLA]
Cost of Living Adjustment to Satellite
Carrier Compulsory License Royalty
Rates
Copyright Royalty Board,
Library of Congress.
ACTION: Final rule.
AGENCY:
The Copyright Royalty Judges
announce a cost of living adjustment
(‘‘COLA’’) of 1.2% in the royalty rates
paid by satellite carriers under the
satellite carrier compulsory license of
the Copyright Act. The COLA is based
on the change in the Consumer Price
Index from October 2009 to October
2010.
SUMMARY:
Effective Date: January 1, 2011.
Applicability Dates: These rates are
applicable for the period January 1,
2011, through December 31, 2011.
FOR FURTHER INFORMATION CONTACT:
Richard Strasser, Senior Attorney, or
Gina Giuffreda, Attorney Advisor.
Telephone: (202) 707–7658. E-mail:
crb@loc.gov.
DATES:
The
satellite carrier compulsory license
establishes a statutory copyright
licensing scheme for the retransmission
of distant television programming by
satellite carriers. 17 U.S.C. 119.
Congress created the license in 1988 and
has reauthorized the license for
additional five-year periods, most
recently with the passage of the Satellite
Television Extension and Localism Act
of 2010, (‘‘STELA’’), Public Law 111–
175, which was signed into law by the
President on May 27, 2010.
Program Suppliers and Joint Sports
Claimants (collectively, the ‘‘Copyright
Owners’’) and DIRECTV, Inc., DISH
Network, LLC, and National
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Programming Service, LLC (collectively,
the ‘‘Satellite Carriers’’) submitted a
voluntary agreement proposing rates for
the section 119 compulsory license for
the period 2010–2014 and requested
that the proposed rates be applied to all
satellite carriers, distributors, and
copyright owners without holding a rate
proceeding. See 17 U.S.C.
119(c)(1)(D)(ii)(I). After publishing the
proposed rates in the Federal Register
and receiving no objections, the Judges
adopted the rates as final in 37 CFR part
386. 75 FR 53198 (August 31, 2010).
Section 119(c)(2) requires the Judges
annually to adjust these rates ‘‘to reflect
any changes occurring in the cost of
living adjustment (for all consumers and
for all items) published * * * before
December 1 of the preceding year’’ with
such rates being effective on January 1
of each year. 17 U.S.C. 119(c)(2). The
Judges are required to publish in the
Federal Register ‘‘[n]otification of the
adjusted fees * * * at least 25 days
before January 1.’’ Id. Today’s notice
fulfills this obligation.
The change in the cost of living as
determined by the CPI–U during the
period from the most recent index
published before December 1, 2009, to
the most recent index published before
December 1, 2010, is 1.2%.1 Rounding
to the nearest cent, the royalty rates for
the secondary transmission of broadcast
stations by satellite carriers for private
home viewing and viewing in
commercial establishments are 25 cents
and 51 cents, respectively.
List of Subjects in 37 CFR Part 386
Copyright, Satellite, Television.
Final Regulations
For the reasons set forth in the
preamble, part 386 of title 37 of the
Code of Federal Regulations is amended
as follows:
■
PART 386—ADJUSTMENT OF
ROYALTY FEES FOR SECONDARY
TRANSMISSIONS BY SATELLITE
CARRIERS
1. The authority citation for part 386
continues to read as follows:
■
Authority: 17 U.S.C. 119(c), 801(b)(1).
2. Section 386.2 is amended by
revising paragraphs (b)(1)(ii) and
(b)(2)(ii) as follows:
■
§ 386.2 Royalty fee for secondary
transmission by satellite carriers.
*
*
*
*
*
1 The most recent CPI–U figures are published in
November of each year and use the period 1982–
1984 to establish a reference base of 100. The index
for October 2009 was 216.177, while the figure for
October 2010 was 218.711.
E:\FR\FM\06DER1.SGM
06DER1
Agencies
[Federal Register Volume 75, Number 233 (Monday, December 6, 2010)]
[Rules and Regulations]
[Pages 75621-75624]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-30399]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 431
Office of Commercial Space Transportation; Waiver of Autonomous
Reentry Restriction for a Reentry Vehicle
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of waiver.
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[[Page 75622]]
SUMMARY: This notice of waiver concerns two petitions for waiver
submitted to the Federal Aviation Administration (FAA) by Space
Exploration Technologies Corp. (SpaceX): A petition to waive the
requirement that a waiver petition be submitted at least sixty days
before the proposed effective date of the waiver, and a petition to
waive the requirement that SpaceX only initiate reentry of its reentry
vehicle, the Dragon Spacecraft (Dragon), by command. The first petition
is unnecessary because, as explained below, SpaceX demonstrated good
cause for its late filing. The FAA finds that waiving the requirement
for SpaceX ground operators to initiate Dragon's reentry to Earth is in
the public interest and will not jeopardize public health and safety,
safety of property, and national security and foreign policy interests
of the United States.
FOR FURTHER INFORMATION CONTACT: For technical questions concerning
this waiver contact Howard Searight, Aerospace Engineer, AST-200,
Office of Commercial Space Transportation (AST), Federal Aviation
Administration, 800 Independence Avenue, SW., Washington, DC 20591;
telephone (202) 267-7927; e-mail: howard.searight@faa.gov. For legal
questions concerning this waiver contact Laura Montgomery, Senior
Attorney for Commercial Space Transportation, AGC-200, Office of the
Chief Counsel, Regulations Division, Federal Aviation Administration,
800 Independence Avenue, SW., Washington, DC 20591; telephone (202)
267-3150; e-mail: laura.montgomery@faa.gov.
SUPPLEMENTARY INFORMATION:
Background: On September 23, 2010, SpaceX requested two waivers
from the FAA's Office of Commercial Space Transportation (AST) for the
reentry of Dragon, a reentry vehicle, to be launched on Falcon 9 flight
002. First, SpaceX requested a waiver of procedural requirements for
waivers set forth at 14 CFR 404.3. Second, SpaceX requested a waiver of
14 CFR 431.43(e)\1\ to allow autonomous reentry.\2\
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\1\ Even though Dragon is a reentry vehicle and not a reusable
launch vehicle, 14 CFR 435.33 incorporates and applies section
431.43 to all reentry vehicles.
\2\ SpaceX stated that autonomous reentry would only be used in
off-nominal circumstances, and the regulation prevents autonomous
reentry only for nominal circumstances, thus rendering a waiver
unnecessary. This interpretation of the regulation conflicts with
the regulation's requirement that an operator only initiate reentry
by command as described in the preamble to the proposed rule. There,
the FAA expressed its concern that authorizing reentry of totally
autonomous vehicles would not fulfill adequately its public safety
responsibility. Without active control, those systems and conditions
necessary for safe reentry would not be verified before reentry was
initiated Commercial Space Transportation Reusable Launch Vehicle
and Reentry Licensing Regulations, 64 FR 19626, 19645 (Apr. 21,
1999) (Reentry NPRM). Because it was the FAA's intent that the
regulations ensure human control capability upon reentry, SpaceX's
petition is a request for a waiver.
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The FAA licenses, in relevant part, the launch of a launch vehicle,
and reentry of a reentry vehicle under authority granted to the
Secretary of Transportation by 49 U.S.C. Subtitle IX, chapter 701
(Chapter 701), and delegated to the FAA's Administrator and Associate
Administrator for Commercial Space Transportation.
SpaceX is a private commercial space flight company. It entered
into a Space Act Agreement with the National Aeronautics and Space
Administration (NASA) as part of NASA's Commercial Orbital
Transportation Services (COTS) program. The COTS program is designed to
stimulate efforts within the private sector to demonstrate safe,
reliable, and cost-effective space transportation to the International
Space Station.
SpaceX's petition for waiver concerns an upcoming demonstration
flight that it plans to undertake as part of the COTS program. At the
time of the filing of the petition, the launch for that flight was
scheduled to take place on November 8, 2010. During the flight,
SpaceX's Falcon 9 vehicle will launch the Dragon reentry vehicle into
orbit. Dragon is a reentry vehicle whose capability SpaceX plans to
demonstrate for NASA. Ultimately, SpaceX intends to use Dragon to
transport cargo and people to and from the International Space Station.
Once Dragon is in orbit, a ground-implemented health check will be
carried out by telemetry. SpaceX has designed the Dragon capsule to
remain in orbit until SpaceX ground operators transmit a reentry
command. A ground operator can issue commands to either enable or
disable the reentry of Dragon based on the health of the vehicle.
Dragon is also able to conduct an autonomous health check. Propellant
and power levels are the key variables used by ground operators in
determining whether to issue commands to reenter or stay in orbit, and
the same variables would be used by the vehicle in its onboard health
check. The onboard health check is designed to check time-dependent
variables to ensure the health and functionality of the propellant,
power and avionics sub-systems. Based on these evaluations, Dragon is
able to determine whether it is healthy. On the ground, the reentry
team can read the raw data and establish for themselves whether Dragon
is healthy. Dragon's onboard health check is designed to replicate the
decision-making process of the ground operators with respect to time-
dependent failures, which are, in Dragon's case, the full depletion of
power and propellant. If Dragon's communications failed and the vehicle
passed the onboard health check, Dragon would reenter autonomously.
Once Dragon passes a ground-implemented health check, ground
operators will issue a reentry command. After ground operators issue
the reentry command, Dragon will wait until the point in space at which
the reentry burn initiation is planned before initiating reentry.
Dragon will reenter, deploy three parachutes and splash down. A nominal
Dragon reentry splashes down in the Pacific Ocean off the coast of
southern California with some propellants on board.
If an anomaly occurs after the issuance of the reentry command,
ground operators can issue a command that disables reentry. SpaceX is
concerned with what would happen if its ground operators were unable to
communicate a reentry command to a healthy Dragon due to failed or
disabled communications. In this circumstance, SpaceX proposes that the
FAA permit the autonomous reentry of a healthy Dragon at the nominal
landing location in order to maximize public safety. This scenario may
play out in different ways. If ground operators needed more time to
complete a health check than that available during one orbit, they
could disable reentry by command. Dragon would then not reenter, even
if its autonomous health check would otherwise allow it to. If a health
check proved satisfactory, ground operators could re-enable reentry,
and Dragon would reenter. If Dragon never received a command, it could
rely on the results of its own continuous autonomous health check, and,
if those results were positive, reenter.
Dragon has several safety features that would allow for a safe
autonomous reentry in the event of a communications failure, including:
(1) The vehicle automatically reduces itself to its lowest energy level
in the case of an off-nominal burn; (2) the vehicle has the ability to
autonomously guide itself to the same pre-determined landing site,
located more than 780 kilometers from the coastline; (3) the vehicle
has the ability to monitor its safety-critical systems in real-time;
(4) the vehicle has over 100% margin on both power and propellant
budgets; (5) the vehicle has a space-grade inertial measurement unit
(IMU); (6) the vehicle
[[Page 75623]]
has a space-grade flight computer; and (7) the vehicle has redundant
drogue parachutes and dual redundant main parachutes.
Waiver Criteria: Chapter 701 allows the FAA to waive a requirement
for an individual license applicant if the FAA decides that the waiver
will not jeopardize public health and safety, safety of property, and
national security and foreign policy interests of the United States and
is in the public interest. 49 U.S.C. 70105(b)(3) (2010); 14 CFR
404.5(b) (2010).
Section 404.3 Waiver Petition
Section 404.3(b)(5) requires that a petition for waiver be
submitted at least sixty days before the proposed effective date of the
waiver. However, this section also provides that a petition may be
submitted late if the petitioner shows good cause. Id. (b)(5).
Here, SpaceX submitted its waiver petition on September 23, 2010,
which was less than sixty days before the November 8, 2010 launch date
planned at the time of the filing of the petition. However, in its
petition, SpaceX explained that it initially interpreted the applicable
regulations differently than the FAA, and was not aware that a waiver
would be required. Once the FAA informed SpaceX that it needed to
obtain a waiver, SpaceX proceeded to apply for the waiver in a timely
fashion. As such, the FAA has found that SpaceX had good cause for
submitting its waiver petition less than sixty days from its launch
date. Therefore, SpaceX's late submission does not violate 404.3(b)(5),
and a waiver of that section is unnecessary.
Section 431.43(e) Waiver Petition
Section 431.43(e) requires, in pertinent part, any operator of a
reusable launch vehicle that enters Earth orbit to issue a command
enabling reentry flight of the vehicle. It further states that reentry
flight cannot be initiated autonomously under nominal circumstances
without prior enable. 14 CFR 431.43(e).
For reasons described below, the FAA waives the requirement of 14
CFR 431.43(e), and allows SpaceX to autonomously initiate reentry
flight of Dragon in the event that SpaceX ground operators lose
communication with Dragon, and Dragon is healthy. In this context,
communication loss means Dragon fails to send a reentry request to
SpaceX's ground operators, or the ground operators are unable to send a
command enabling reentry of Dragon. The onboard health check is
designed to check time-dependent variables to ensure the health and
functionality of the propellant, power and avionics sub-systems.
In deciding whether or not to waive the requirement that Dragon's
operator issue a command to enable reentry of the vehicle, the FAA must
analyze whether the waiver: (1) Is in the public interest; (2) will not
jeopardize public health and safety or safety of property; and (3) will
not jeopardize national security and foreign policy interests of the
United States. 49 U.S.C. 70105(b)(3); 14 CFR 404.5(b). The FAA will
grant this waiver because SpaceX satisfies the criteria.
A. Public Interest
The change proposed by SpaceX is consistent with the statutory goal
of seeking improvements to safety. 49 U.S.C. 70101(a)(12) and
(b)(2)(C). Granting SpaceX's waiver is in the public interest because a
guided reentry is safer than a random reentry, and therefore Dragon's
proposed autonomous reentry capability enhances the overall safety of
the mission.
B. Public Health and Safety
Although the FAA's regulation prohibits autonomous reentry, a
waiver is warranted in SpaceX's case because an autonomous reentry of a
healthy Dragon that has lost ground communications is safer than a
random reentry. The preamble to the Reentry NPRM acknowledges that some
RLV operators were contemplating totally autonomous reentry capability,
and expressed a concern that autonomous reentry was not adequately
safe. Specifically, the FAA was concerned about system anomalies or
other non-compliant conditions that would not be verified before
initiation of reentry in the absence of active human control. Reentry
NPRM, 64 FR at 19645. The FAA retained flexibility in granting waivers
to allow the use of autonomous systems. Commercial Space Transportation
Reusable Launch Vehicle and Reentry Licensing Regulations, 65 FR 56618,
56641 (Sept. 19, 2000) (Reentry Rule). In requiring the capability for
human intervention, the FAA did not intend to foreclose the use of
autonomous systems or autonomous decision-making. Id. SpaceX's proposed
approach addresses the concern underlying the regulatory requirements
and poses less risk than that associated with Dragon being left in
orbit to reenter randomly at some later time. SpaceX's mitigation
measures are of additional importance to the FAA's decision to grant a
waiver.
The FAA's reason for requiring commanded reentry was to make sure
that an operator had the chance to verify that there were no system
anomalies or other non-compliant conditions. Under SpaceX's proposed
plan, the operator would employ two means of detecting any such
anomalies. Ground operators and Dragon's own continuous autonomous
health check would both perform health checks to determine whether
conditions prohibited reentry.
To determine the effect of granting SpaceX's waiver on public
safety, the FAA performed a risk analysis of potential reentry
outcomes. The risks of leaving the vehicle in orbit or attempting a
reentry (whether autonomous or commanded) are best compared by applying
conditional probabilities, where an undesired event is assumed to
happen, to each possibility. For purposes of comparison, in the two
cases discussed below, the FAA assumes that Dragon fails to expel its
propellant, and its parachutes fail to deploy, resulting in an
explosive impact.
In a random reentry scenario, Dragon has lost communications and is
unable to reenter autonomously. The FAA assumed a 100% probability of
leaving the vehicle in orbit with a full propellant load. The vehicle
would continue circling the Earth until it reentered randomly due to
natural orbital decay. The FAA assumed the impact probability in a
given latitude band was equivalent to the dwell time of the vehicle in
orbit over that latitude band. The FAA computed the population density
as a function of latitude by dividing the population within each
latitude band under Dragon by the Earth's surface area within each
latitude band. The FAA applied a sheltering model based on surveys and
socioeconomic factors, including population density and distribution
and the types of homes people live in, all of which affect expected
casualties. The conditional risk computed for a random reentry produced
an expected average number of casualties (Ec) of
approximately 23 x 10-3.
In an autonomous reentry scenario, Dragon has lost communications
and is attempting an autonomous reentry. The FAA assumed a 100%
probability of reentry burn failure at any time from burn initiation to
burn cutoff, assuming a uniform failure rate. In this scenario, Dragon
remains orbital for two-thirds of its burn. Two-thirds of the
conditional random reentry risk calculated above results in an
Ec of approximately 15 x 10-3. The remaining risk
results from an assumed failure during the last third of the reentry
burn when the vehicle is no longer in orbit. This results in a flight
corridor extending from the Atlantic to the Pacific crossing over the
continental
[[Page 75624]]
United States and Northern Mexico. The conditional risk along this
flight corridor is approximately Ec 13 x 10-3.
The FAA multiplied 13 x 10-3 by one-third, to account for
the fact that this failure mode is only applicable to one-third of the
burn, which results in an Ec of 41 x 10-4. The
total conditional risk associated with an autonomous reentry, where a
burn failure is assumed, is 19 x 10-3. Thus, there is
theoretically 20% less risk in an attempt to reenter Dragon than there
is in leaving it in orbit given a communications failure.
Also of importance to the FAA's decision to grant a waiver, Dragon
is equipped with a number of mitigating features. First, the vehicle
automatically safes itself in the case of an off-nominal burn. This
means that if Dragon conducted its reentry burn, but computed that the
desired landing spot would not be achieved, it would vent the rest of
its fuel, thereby reducing the possibility of explosion or dispersion
of toxic fumes on impact. Second, the vehicle has the ability to
autonomously guide itself to its planned landing location in the
Pacific Ocean, some 780 kilometers from the coastline. This internal
capability allows Dragon to act independently, based on programmed
instructions and information regarding its location, if communications
with the ground are lost. Third, the vehicle has the ability to monitor
its safety-critical systems in real-time. This means Dragon has near-
immediate awareness of the operability of its on-board systems that
allow it to operate safely, and this awareness enables Dragon to react
in time to conduct a reentry. Fourth, the vehicle has a space-grade IMU
and flight computer. This means Dragon is equipped with a system that
provides information on where Dragon is, which is pertinent to its
guidance capabilities, and the IMU and flight computer are designed and
tested to operate in the rigorous conditions of space.
C. National Security and Foreign Policy Implications
The FAA has not identified any national security or foreign policy
implications associated with granting this waiver.
Summary and Conclusion: A waiver is in the public interest because
it accomplishes the goals of Chapter 701 and decreases risk to the
public. The waiver will not jeopardize public health and safety or
safety of property because allowing autonomous reentry of a healthy
Dragon vehicle that has lost all communications presents less risk than
a random reentry. A waiver will not jeopardize national security and
foreign policy interests of the United States. For the foregoing
reasons, the FAA has waived the requirement of 14 CFR 431.43(e) for a
commanded reentry, and allows SpaceX to autonomously initiate reentry
flight of Dragon in the event that all communication between ground
operators and Dragon has been lost, and Dragon is healthy.
Issued in Washington, DC on November 30, 2010.
Kenneth Wong,
Licensing and Safety Division Manager.
[FR Doc. 2010-30399 Filed 12-3-10; 8:45 am]
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