Experimental Licensing System

0019-EX-ST-2013

Orbital Sciences Corporation

Filing overview

StatusGrant Expired Due to New License
Call signWG9XGU
Filed2013-01-08
Status date2013-03-29
FCC sourceView the FCC filing record

Special Temporary Authority application - Address

Attention:
Chennault Slaughter
City:
Chandler
E-Mail Address:
[email protected]
State:
AZ
Street Address:
3380 S. Price Rd
Zip Code:
85248

Special Temporary Authority application - Applicant Name

Name of Applicant:
Orbital Sciences Corporation

Special Temporary Authority application - Best Contact

First Name:
Chennault
Last Name:
Slaughter
Phone Number:
480-814-6076
Title:
Principal Electrical 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:
2013-01-08 00:00:00.0
Signature of Applicant (Authorized person filing form):
Chennault Slaughter
Title of Applicant (if any):
Principal Electrical Engineer

Special Temporary Authority application - Explanation

Please explain in the area below why an STA is necessary:
Orbital Sciences Corporation will utilize the Minotaur I Launch Vehicle to deliver the ORS-3 spacecraft to low earth orbit as part of the Air Force Space Development and Test Directorates Operational Responsive Space program. The launch mission requires vehicle-to-ground communicationfrom launch until payload is delivered into low earth orbit. The Air Force is directing Orbital to request an STA to license the radio frequency emitters on the launch vehicle to cover emissions during the short duration of the mission.

Special Temporary Authority application - Information

Callsign:
WG9XGU
Class of Station:
MO
Nature of Service:
Experimental

Special Temporary Authority application - Initial values - Purpose of Operation

Please explain the purpose of operation:
Orbital Sciences Corporation will utilize the Minotaur I Launch Vehicle to deliver the ORS-3 spacecraft into low earth orbit. Radio frequency emitters on the launch vehicle serve 2 purposes for operation. One purpose is to provide telemetry, which is used to monitor launch vehicle health and status and to communicate the inertial guidance position of the launch vehicle. The other purpose is to support range tracking by way of a transponder that is interrogated from the ground.

Special Temporary Authority application - Manufacturer

Equipment 1 Experimental
No
Equipment 1 Manufacturer
L3/COM
Equipment 1 Model Number
ST20055
Equipment 1 No. Of Units
2
Equipment 2 Experimental
No
Equipment 2 Manufacturer
Herley
Equipment 2 Model Number
MD400C-2
Equipment 2 No. Of Units
1

Special Temporary Authority application - Purpose of Operation

Please explain the purpose of operation:
Launch Vehicle testing Orbital Sciences Corporation will utilize the Minotaur I Launch Vehicle to deliver the ORS-3 spacecraft into low earth orbit. Radio frequency emitters on the launch vehicle serve 2 purposes for operation. One purpose is to provide telemetry, which is used to monitor launch vehicle health and status and to communicate the inertial guidance position of the launch vehicle. The other purpose is to support range tracking by way of a transponder that is interrogated from the ground.

Special Temporary Authority application - Requested Period of Operation

Operation End Date:
12/15/2013
Operation Start Date:
06/15/2013

Frequencies

ActionLower MHzUpper MHzClassOutput WERP WEmissionSignal
Virginia
Virginia
StateRadius of Operation
New2239.760000002243.24000000MO5.0000004.6000003M48F1D1.05 MHz peak deviation
New2286.760000002290.24000000MO5.0000002.6000003M48F1D1.05 MHz peak deviation
New5758.000000005772.00000000MO400.000000400.00000014M0P0N0.5 microsecond pulse

Sites

SiteLocationCoordinatesCountyRadius
VirginiaNorth 37 49 52 West 75 29 29
VirginiaNorth 37 49 52 West 75 29 29

Grant actions

DateCategoryDescription
2013-09-20GrantGrant Generated [Sep 20 2013]
2013-03-29GrantGrant Generated [Mar 29 2013]

Documents

DocumentTypeDateStatus
Grant E-mail Notification generated [Mar 30 2013]Correspondence2013-03-30Available
Mission Nominal TimelineText Documents2013-03-20Available
Power Spectral DensityText Documents2013-03-20Available
Trajectory Data FileText Documents2013-03-20Available
ORS TM EIRP ResultsText Documents2013-03-20Available
Ground StationsText Documents2013-03-20Available
View GrantAvailable
View GrantAvailable

Sources and provenance

SourceSource recordRetrievedMatch
ELS0019-EX-ST-20132026-07-30 08:56:00Source Primary

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