Orbital ATK , Inc.

0960-EX-ST-2017

Status: Grant Expired Due to New License

WL9XZA
2017-12-14

Documents and Communications: [refresh]

DescriptionCategoryDate
Response 7/31Correspondence2017-08-01
E-Mail generated [Jul 31 2017]Correspondence2017-07-31
Grant E-mail Notification generated [Nov 1 2017]Correspondence2017-11-01
Attachment 3 Ground StationsText Documents2017-08-14
Attachment 4 Debris Assessment ReportText Documents2017-08-14
Application Form:
OET Special Temporary Authority Report
FEDERAL COMMUNICATIONS COMMISSION
APPLICATION FOR SPECIAL TEMPORARY AUTHORITY

Applicant Name
Name of Applicant:  Orbital ATK , Inc.

Address
Attention: Mr. Michael McGovern
Street Address: 45101 Warp Drive
P.O. Box:
City: Dulles
State: VA
Zip Code: 20166
Country: United States
E-Mail Address: [email protected]

Best Contact
Give the following information of person who can best handle inquiries pertaining to this application:  
Last Name: Delahaye
First Name: Derrick
Title: RF Communications Systems Engineer
Phone Number: 703-406-5834

Explanation
Please explain in the area below why an STA is necessary:
Orbital Sciences Corporation (Orbital) will launch and operate the OA-8 Cygnus spacecraft as part of the NASA Cargo Resupply Services (CRS) program. The Cygnus mission will include launch, orbit raising maneuvers, approach and berthing with the International Space Station (ISS), unberthing and departure from the ISS, orbit maneuvering, and destructive re-entry into the Earth’s atmosphere. Destructive re-entry is anticipated to be up to 14 days after separation from the ISS. During the period between ISS departure and re-entry, the Cygnus spacecraft will deploy cubesats. Spacecraft telemetry is transmitted during all phases of mission operations. An STA is requested at the direction of NASA and the NTIA due to the short duration of the mission and the need for close coordination within the necessary frequency bands. This STA is consistent with the FCC/NTIA policies developed during the STA application process for both the OA-6 and OA-7 Cygnus spacecrafts. See FCC File Number 1334-EX-ST-2015 and 1709-EX-ST2016 respectively.

Purpose of Operation
Please explain the purpose of operation:  Spacecraft telemetry links for monitoring of Cygnus spacecraft state of health. Telemetry links include: 1) S-Band Single Access (SSA) spread spectrum return link operation with NASA TDRSS 2) High data rate downlink operation with mission Ground Stations 3) A Cygnus to ISS link for proximity operations will be used during the mission. The transmitters supporting these links are described below: The Cygnus spacecraft configuration will comprise of two Quasonix radios operating at 2287.5 MHz in TDRSS SSA mode and it will also provide telemetry downlinks at 3 Mbps and 6 Mbps. The Quasonix radios have the same radio design as the radios used on the OA-6 and OA-7 missions. These radios will meet all STA parameters and conditions as compiled with the two previous CRS STA applications.

Information
Callsign: WL9XZA
Class of Station: MO
Nature of Service: Experimental

Requested Period of Operation
Operation Start Date: 10/27/2017
Operation End Date: 04/27/2018

Manufacturer
List below transmitting equipment to be installed (if experimental, so state) if additional rows are required, please submit equipment list as an exhibit:  
Manufacturer Model Number No. Of Units Experimental
Quasonix 6354-PF4510-08 2 Yes
Mitsubishi Electrical Company 6341-PF4523-01 2 Yes

Certification
Neither the applicant nor any other party to the application is subject to a denial of Federal benefits that includes FCC benefits pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 U.S.C. Section 862, because of a conviction for possession or distribution of a controlled substance. The applicant hereby waives any claim to the use of any particular frequency or electromagnetic spectrum as against the regulatory power of the United States because of the prvious use of the same, whether by license or otherwise, and requests authorization in accordance with this application. (See Section 304 of the Communications Act of 1934, as amended.) The applicant acknowledges that all statements made in this application and attached exhibits are considered material representations, and that all the exhibits part hereof and are incorporated herein as if set out in full in this application; undersigned certifies that all statements in this application are true, complete and correct to the best of his/her knowledge and belief and are made in good faith. Applicant certifies that construction of the station would NOT be an action which is likely to have a significant environmental effect. See the Commission's Rules, 47 CFR1.1301-1.1319.
Signature of Applicant (Authorized person filing form): Derrick Delahaye
Title of Applicant (if any): RF Communication Systems Engineer
Date: 2017-07-11 00:00:00.0

Station Location
City State Latitude Longitude Mobile Radius of Operation
North      West      Spacecraft-350km altitude-51.6 degrees inclination
Datum:  NAD 83
Is a directional antenna (other than radar) used?   No
Exhibit submitted:   No
(a) Width of beam in degrees at the half-power point:  
(b) Orientation in horizontal plane:  
(c) Orientation in vertical plane:  
Will the antenna extend more than 6 meters above the ground, or if mounted on an existing building, will it extend more than 6 meters above the building, or will the proposed antenna be mounted on an existing structure other than a building?   No
(a) Overall height above ground to tip of antenna in meters:  
(b) Elevation of ground at antenna site above mean sea level in meters:  
(c) Distance to nearest aircraft landing area in kilometers:  
(d) List any natural formations of existing man-made structures (hills, trees, water tanks, towers, etc.) which, in the opinion of the applicant, would tend to shield the antenna from aircraft:
Action Frequency Station Class Output Power/ERP Mean Peak Frequency Tolerance (+/-) Emission Designator Modulating Signal
Modified 2205.00000000- MHz MO 1.860000 W 1.080000 W M 0.00045000 % 4M20G1D SS-UQPSK
Action Frequency Station Class Output Power/ERP Mean Peak Frequency Tolerance (+/-) Emission Designator Modulating Signal
Modified 2287.50000000- MHz MO 13.190000 W 3.330000 W M 0.00003000 % 6M16G1D SQPN
Action Frequency Station Class Output Power/ERP Mean Peak Frequency Tolerance (+/-) Emission Designator Modulating Signal
Modified 2287.50000000- MHz MO 13.190000 W 3.330000 W M 0.00003000 % 4M98G1D SQPSK
Action Frequency Station Class Output Power/ERP Mean Peak Frequency Tolerance (+/-) Emission Designator Modulating Signal
Modified 2287.50000000- MHz MO 13.190000 W 3.330000 W M 0.00003000 % 3M00G1D SQPSK

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