Attachment Supplement

This document pretains to SES-AMD-20100416-00448 for Amended Filing on a Satellite Earth Station filing.

IBFS_SESAMD2010041600448_810978

                 SUPPLEMENT TO ORBITAL DEBRIS MITIGATION SHOWING


            Attached hereto is information regarding the end-of-life status of the propellant,

oxidizer and helium tanks on APSTAR VI.          The propellant and oxidizer tanks will be vented


at end-of-life by leaving the thruster valve open. The three helium tanks, however, are sealed

and will have a total estimated mass of 6.6 kilograms of helium remaining at the end-of-life.


Information on the volume, pressure and assumed temperature of the helium tanks is attached

hereto.


           To the extent necessary, a waiver of the requirement in Section 25.283(a) of the FCC’s

Rules that pressure vessels be relieved at end-of-life is hereby requested in connection with


the three sealed helium tanks on APSTAR VI. It should be noted that APSTAR VI was

launched in April 2005, which is a relatively short time after the September 9, 2004, Federal


Register publication date of Section 25.283. Moreover, the Satellite Industry Association

(“SIA”), along with a number of satellite operators, manufacturers, and service providers,


have proposed that the FCC grant a blanket waiver of Section 25.283(c) for in-orbit satellites,

such as APSTAR VI, that cannot fully comply with the rule. Such a limited waiver is


warranted in light of the proposed service that can be provided by APSTAR VI and the

impossibility of changing APSTAR VI’s design at this time.




{00167086-1 }


                 Assessments on Conformity of APSTAR-VI Satellite

                                       with FCC rules

                          Regarding Orbital Debris Mitigation

         Regarding the question for propulsion system for APSTAR VI, that the
         additional information in respect of helium remaining with the pressure,
         container and volume are stated as the below:‐




                                 APSTAR-VI(SB4000C2)
                  container                 status on end of life
                      1     fuel     vent by leaving thruster valve open
                      2     oxidizer vent by leaving thruster valve open
                      3     helium     sealed: 51.6litre,30bar,0-40°C
                      4     helium     sealed: 51.6litre,30bar,0-40°C
                      5     helium     sealed: 51.6litre,30bar,0-40°C




{00167086­1 }
                                               1
                                                                              18 August,2009



Document Created: 2010-04-15 17:50:05
Document Modified: 2010-04-15 17:50:05

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