ODAR Update Letter 0

LETTER submitted by Hiber, Inc.

Letter

2019-03-01

This document pretains to SAT-PDR-20180910-00069 for Petition for Declaratory Ruling on a Satellite Space Stations filing.

IBFS_SATPDR2018091000069_1631845

                                                                                                             Hogan Lovells US LLP
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March 1, 2019

VIA ELECTRONIC FILING

Ms. Marlene H. Dortch
Secretary
Federal Communications Commission
445 12th Street S.W.
Washington, D.C. 20554


Re:          Hiber, Inc., Supplement to Orbital Debris Assessment Report
             IBFS File No. SAT-PDR-20180910-00069; Call Sign S3038

Dear Ms. Dortch:

Hiber, Inc. (“Hiber”), through its counsel, submits this letter to update its orbital debris assessment
report (“ODAR”) submitted on February 22, 2019.1 In Section 3.7 of the ODAR, Hiber calculated that
two components of spacecraft were expected to survive reentry, the S-band antenna and the GPS
antenna. With respect to the S-band antenna, Hiber had erroneously based its calculations
assuming the antenna is made of ceramic when, in fact, the S-band antenna is made of anodized
aluminum. Recalculating the reentry analysis using the correct material shows that the S-band
antenna does not survive reentry. With respect to the GPS antenna, Hiber recalculated the impact
energy for the GPS antenna using more precise measurements for its mass, rather than the worst-
case assumptions originally used, and determined that the impact energy of the antenna with the
more precise mass value is 7.62 joules, which is below the 15-joule NASA threshold.2

If you have any questions regarding this letter, please do not hesitate to contact me.

Very truly yours,

/s/Tony Lin

Tony Lin
Counsel to Hiber, Inc.

cc:          Karl Kensinger
             Stephen Duall



1
  See Letter from Lynne Montgomery, Counsel to Hiber, Inc., to Jose Albuquerque (February 22,
2019).
2
  See NASA Technical Standard, Process for Limiting Orbital Debris, NASA-STD-8719.14A (with
Change 1) (May 25, 2012). Although not stated in the ODAR, using the worst-case mass
assumption, the impact energy associated with the GPS antenna was calculated to be ~18 joules.
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Document Created: 2019-03-01 08:49:55
Document Modified: 2019-03-01 08:49:55

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