Experimental Licensing System

0307-EX-ST-2019

Orbital Sciences Corporation

Filing overview

StatusGrant Expired Due to New License
Call signWO9XDR
Filed2019-02-26
Status date2019-03-21
FCC sourceView the FCC filing record

Special Temporary Authority application - Address

Attention:
DS LAW PLLC
City:
Washington
E-Mail Address:
[email protected]
State:
DC
Street Address:
1629 K St NW Ste 300
Zip Code:
20166

Special Temporary Authority application - Applicant Name

Name of Applicant:
Orbital Sciences Corporation

Special Temporary Authority application - Best Contact

First Name:
Derrick
Last Name:
Delahaye
Phone Number:
703-406-5834
Title:
RF Communications Systems Engineer

Special Temporary Authority application - Certification

Applicant 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.
Date:
2019-02-26 00:00:00.0
Signature of Applicant (Authorized person filing form):
Derrick Delahaye
Title of Applicant (if any):
RF Communications Systems Engineer

Special Temporary Authority application - Explanation

Please explain in the area below why an STA is necessary:
Orbital Sciences Corporation, a wholly owned subsidiary of Northrop Grumman Innovation Systems, Inc. (NGIS) will launch and operate the NG-11 Cygnus spacecraft as part of the NASA Commercial 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, followed by orbit maneuvering, and finally controlled destructive re-entry into the Earths atmosphere. Destructive re-entry is anticipated to be up to 9 months after separation from the ISS. We plan to apply for an extension to support the duration in orbit beyond the initial six months. During the period between ISS departure and re-entry, the Cygnus spacecraft will utilize a NanoRacks CubeSat Satellite Deployer (NRCSD) to deploy microsats. The cubesats owners are responsible for obtaining their STA. Spacecraft telemetry is transmitted during all phases of mission operations. An STA is requested for the Cygnus spacecraft 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 previous CRS Cygnus spacecrafts.

Special Temporary Authority application - Information

Callsign:
WO9XDR
Class of Station:
MO
Nature of Service:
Experimental

Special Temporary Authority application - Initial values - Explanation

Please explain in the area below why an STA is necessary:
Orbital Sciences Corporation, a wholly owned subsidiary of Northrop Grumman Innovation Systems, Inc. (NGIS) will launch and operate the NG-11 Cygnus spacecraft as part of the NASA Commercial 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, followed by orbit maneuvering, and finally controlled destructive re-entry into the Earths atmosphere. Destructive re-entry is anticipated to be up to 10 months after separation from the ISS. During the period between ISS departure and re-entry, the Cygnus spacecraft will utilize a NanoRacks CubeSat Satellite Deployer (NRCSD) to deploy microsats. The cubesats owners are responsible for obtaining their STA. Spacecraft telemetry is transmitted during all phases of mission operations. An STA is requested for the Cygnus spacecraft 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 previous CRS Cygnus spacecrafts.

Special Temporary Authority application - Manufacturer

Equipment 1 Experimental
Yes
Equipment 1 Manufacturer
L-3 Cincinnati Electronics
Equipment 1 Model Number
6354-PF4520-01
Equipment 1 No. Of Units
2
Equipment 2 Experimental
Yes
Equipment 2 Manufacturer
L-3 Cincinnati Electronics
Equipment 2 Model Number
6354-PF4520-02
Equipment 2 No. Of Units
2

Special Temporary Authority application - 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) and S-Band Multiple Access (SMA) spread spectrum return link operation with NASA TDRS. 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 L-3 Cincinnati Electronics (L-3 CE) transmitters (primary & redundant-backup) operating at 2287.5 MHz in TDRS mode and it will also provide telemetry downlinks at 3 Mbps and 6 Mbps. Two additional transmitters (primary & redundant-backup), also procured from L-3 CE, operating at 2203.2 MHz will be used for the Cygnus to ISS proximity communication link. These transmitters will meet all STA parameters and conditions as compiled with previous CRS STA applications.

Special Temporary Authority application - Requested Period of Operation

Operation End Date:
10/10/2019
Operation Start Date:
04/10/2019

Frequencies

ActionLower MHzUpper MHzClassOutput WERP WEmissionSignal
NewMO15.4500004.0000003M00G1DSQPSK
ModifiedMO15.4500004.0000003M00G1DSQPSK
NewMO15.4500004.0000004M98G1DSQPSK
ModifiedMO15.4500004.0000004M98G1DSQPSK
NewMO14.6200007.1600005M93G1DSQPN
ModifiedMO14.6200007.1600005M93G1DSQPN
ModifiedMO23.3300006.0400006M16G1DSQPN
NewMO15.4500004.0000006M16G1DSQPN
ModifiedMO15.4500004.0000006M16G1DSQPN
NewMO23.3300006.0400006M16G1DSQPN

Sites

SiteLocationCoordinatesCountyRadius
North West

Grant actions

DateCategoryDescription
2019-03-21GrantGrant Generated [Mar 21 2019]

Notes

DateComment
2019-03-21Experimental Radio License STA for the NG-11 Cygnus spacecraft flight operations.

Documents

DocumentTypeDateStatus
Grant E-mail Notification generated [Mar 22 2019]Correspondence2019-03-22Available
Launch SiteText Documents2019-03-05Available
Attachment 3 correctedText Documents2019-02-26Available
Attachment 4Text Documents2019-02-26Available
Attachment 3Text Documents2019-02-26Available
Attachment 3Text Documents2019-02-26Available
Attachment 1Text Documents2019-02-26Available
Attachment 2Text Documents2019-02-26Available
View GrantAvailable

Sources and provenance

SourceSource recordRetrievedMatch
ELS0307-EX-ST-20192026-07-30 08:56:45Source Primary

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