Attachment STA Narrative

This document pretains to SAT-STA-20140922-00103 for Special Temporal Authority on a Satellite Space Stations filing.

IBFS_SATSTA2014092200103_1061889

                                    Before the
                     FEDERAL COMMUNICATIONS COMMISSION
                              Washington, D.C. 20554


In the Matter of Request of                          )
                                                     )
XM RADIO LLC                                         )   Call Sign S2119
                                                     )
For Special Temporary Authority to                   )
Extend the XM-2 License Term and                     )
Revise the Orbital Debris Mitigation Plan            )

Expedited Action Requested


                 REQUEST FOR SPECIAL TEMPORARY AUTHORITY

               XM Radio LLC (“XM Radio”) respectfully requests special temporary authority

(“STA”) for a period of 30 days commencing on September 27, 2014, to extend the license term

for the XM-2 space station and permit its removal to a disposal orbit pursuant to a revised orbital

debris mitigation plan that reflects a higher level of residual xenon. Grant of the requested

authority will serve the public interest by facilitating the orderly retirement of XM-2 beginning

in October.

               XM-2 commenced operations at 115° W.L. on March 31, 2001, with an initial

eight-year license term. However, due to performance issues, the satellite was replaced as a

primary operational satellite at 115° W.L. in October 2006, when XM Radio launched XM-4. 1

Earlier this year, XM Radio sought and obtained STA to extend the XM-2 license term, which

was due to expire on March 31, 2014, and to permit relocation of XM-2 to 27° W.L. with an

1
     When launched, XM-2 had an expected useful life of fifteen years. In late August 2001,
Boeing Satellite Systems (“BSS”), the satellite manufacturer, advised XM Radio of a progressive
degradation problem with the solar array output power of the first generation BSS 702 class
satellites, including XM-2. XM Radio accelerated the replacement of XM-2 in response to this
issue.


east-west stationkeeping tolerance of +/- 0.1 degrees in preparation for orbit-raising maneuvers. 2

Subsequent to grant of the XM-2 STA Request, XM Radio has been taking the planned steps to

ready the spacecraft for retirement, drifting the satellite to 27° W.L. and venting excess

propellant onboard the spacecraft, which has both a traditional liquid bi-propellant system that

was used for initial orbit raising and an electric xenon ion propulsion system (“XIPS”) used for

stationkeeping while in orbit.

               The XM-2 STA Request did not propose any changes to the approved orbital

debris mitigation plan for the spacecraft. 3 In that STA application, however, XM Radio

emphasized that XM-2 is the first spacecraft in the BSS 702 product line to be removed to a

disposal orbit and neither BSS itself nor any other satellite operator had prior experience venting

the XIPS systems. 4 Based on XM Radio’s newly acquired experience with XIPS venting the

company has had to revise its plans. Specifically, although venting the bi-propellant system will

be complete in mid-October, XM Radio has not been able to deplete the excess xenon on board

the spacecraft as quickly as anticipated. As a result, if the orbit-raising maneuvers begin as

scheduled on or about October 15, the residual xenon on XM-2 after its retirement would exceed

the amounts specified in the Commission-approved orbital debris plan for the spacecraft. XM

Radio seeks Commission authorization to proceed with the updated orbital debris mitigation plan

set forth herein to permit orbit-raising to commence according to the current schedule.




2
    See Call Sign S2119, File No. SAT-STA-20140204-00018, (the “XM-2 STA Request”),
grant-stamped Mar. 28, 2014.
3
    See id., Narrative at 3.
4
    See id., Narrative at 2.


                                                 2


               XM Radio previously submitted information provided by BSS indicating that

approximately 2.2 kg (2200 grams) of xenon would remain in each of the two xenon tanks

onboard XM-2 at end of life. 5 Based on this data and given the fact that XM-2 was designed and

launched prior to the Commission’s adoption of its orbital debris mitigation requirements, the

Commission granted XM Radio a waiver of the Section 25.283(c) requirements to vent excess

propellant and relieve pressure vessels in connection with the residual xenon expected to be on

XM-2 at end of life. 6 While the pressure in the xenon tanks will be relieved, XM Radio now

projects that 18-22 kg of residual xenon will remain in each tank at end of life. As set forth

below, approving the revised plan with respect to residual xenon and granting an updated waiver

of Section 25.283(c) would be in the public interest in light of the specific facts here.

               A number of factors have contributed to the change in the projected end of life

xenon levels for XM-2. As a threshold matter, because XM-2 is being retired early due to

performance issues outside of XM Radio’s control, the amount of xenon used during the

satellite’s operational lifetime was reduced, leading to a higher level of residual xenon as a

starting point. XM Radio had planned to vent the excess xenon while XM-2 was positioned at

27° W.L., but that process has proved to take significantly longer than had been expected.

               As noted above, the XIPs system on XM-2 is used for regular stationkeeping

maneuvers. This means that after a period of time venting xenon each day, the system must be

reconfigured to operate in stationkeeping mode. XM Radio found that the reconfiguration


5
    See Call Sign S2119, File No. SAT-MOD-20101001-00205, Technical Appendix at 4
(explaining that the xenon tanks are equipped with a regulator that prevents additional gas from
being vented once the pressure falls below the set point of the regulator), grant-stamped Nov. 9,
2010.
6
    See id., Attachment to Grant at 2, ¶ 6.


                                                  3


process was much more complicated and time-consuming than it had anticipated, with the result

that the time that could be spent venting the xenon each day was reduced.

                Continuing to vent xenon after the satellite is decommissioned is not possible. As

XM Radio has explained, reliable ground resources operating with the S- and X-band

frequencies used by XM-2 and the tracking capabilities needed to support the orbit-raising

maneuvers and decommissioning are extremely limited. 7 As a result, once the orbit-raising

begins, XM Radio will have a restricted window of time before the satellite’s westward drift

takes it beyond the range of the ground network. The decommissioning process includes sending

commands to the satellite to drain the batteries and turn off all active units, and these steps must

be taken before the ground antennas lose contact with the satellite. Because opening the valves

to the xenon tanks requires power, the valves will close and remain closed once the power to the

satellite is terminated.

                Maintaining XM-2 at 27° W.L. to vent additional xenon before beginning orbit-

raising maneuvers would materially delay the satellite’s retirement. Rather than being able to

commence the retirement process in mid-October as planned, XM Radio would have to put off

the orbit-raising until mid-April of 2015, given the length of time it would take to significantly

reduce the xenon levels and the delay required by the spring eclipse season. 8 Moreover, because

uncertainty regarding the amount of xenon remaining in the tanks is higher than was originally

forecast, a greater reserve of xenon is needed to ensure the target disposal orbit parameters can




7
    XM-2 STA Request, Narrative at 2-3.
8
     These delays would also affect the timetable for XM-1’s retirement, which cannot begin
until after orbit-raising for XM-2 is completed given the need to use the same limited ground
antenna resources.


                                                  4


be achieved. Therefore, even with additional time for venting, XM Radio would be projecting

higher residual xenon levels than those specified in its prior orbital debris mitigation plan.

               Instead, XM Radio seeks Commission authority to proceed with retirement of

XM-2 as currently scheduled starting in mid-October 2014 and requests a waiver of

Section 25.283(c) to reflect the increased residual xenon. The additional xenon does not increase

the risk of orbital debris. With 18-22 kg of xenon, the pressure in each tank will be 3.7-4.2 MPa

assuming a temperature of 20° Celsius. This pressure represents a small fraction (12-14%) of the

30.1 MPa for which the tanks have been proof pressure tested and will drop further as the

temperature on the spacecraft decreases following shut-down of its electrical systems. Because

the xenon is inert, having the higher levels of residual xenon on board the spacecraft at its end of

life will pose no risk of chemical energy release. Furthermore, the tanks are well shielded and

will be isolated from any source of electrical energy. XM Radio emphasizes that nothing has

changed with respect to XM Radio’s plan to raise XM-2 to a disposal orbit at least 313 km above

the geostationary arc, which is the altitude derived by application of the IADC standard. 9




9
    See File No. SAT-AMD-20080129-00032 (Call Sign S2119), Attachment 1 at 3-4, grant-
stamped Feb. 14, 2008.


                                                  5


               Under these circumstances, the public interest would be served by permitting

retirement of XM-2 to go forward under the current schedule, rather than requiring venting of

additional xenon. Accordingly, XM Radio respectfully requests special temporary authority for

a period of 30 days commencing on September 27, 2014, to extend the XM-2 license term and to

allow retirement of the satellite to proceed in accordance with the updated orbital debris

mitigation plan discussed herein.

                                              Respectfully submitted,

                                              XM Radio LLC

                                              /s/ James S. Blitz
Of Counsel                                    James S. Blitz
Karis A. Hastings                             Vice President, Regulatory Counsel
SatCom Law LLC                                XM Radio LLC
1317 F Street, N.W., Suite 400                1500 Eckington Place, N.E.
Washington, D.C. 20004                        Washington, D.C. 20002
(202) 599-0975                                (202) 380-4000

Dated: September 22, 2014




                                                 6


                                    Technical Certification

              I, Bridget Neville, Vice President and General Manager for Satellite Engineering

and Operations of Sirius XM Radio Inc., hereby certify under penalty of perjury that:

              I am the technically qualified person with overall responsibility for preparation of

the technical information contained in the foregoing STA request. I am familiar with the

technical requirements of Part 25 of the Commission’s rules, and the information contained in

the request is complete and accurate to the best of my knowledge, information and belief.

                                                _________/s/___________
                                                Bridget Neville

Dated: September 22, 2014



Document Created: 2014-09-22 15:22:26
Document Modified: 2014-09-22 15:22:26

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