IBFS / ICFS

SAT-STA-20210208-00018

Astrobotic Technology, Inc

Astrobotic's Peregrine Mission 1 will de

Filing overview

StatusClosed
Applicant FRN0029965993
ContactEduardo Lugo Perez
Filing typeSTA
Date filed2021-02-08
Status date2021-03-19
ServiceSAT
Last actionWithdrawn
FCC sourceView the FCC filing record

Application details

FCC form
FCC Form 312
Application type
APPLICATION FOR SPACE STATION SPECIAL TEMPORARY AUTHORITY

Application summary

Enter a description of this application to identify it on the main menu:
Astrobotic's Peregrine Mission 1 will de

Filing preparer

Filing on Behalf of:
IBFS Service

1. Applicant Information

FRN
0029965993
Name
Astrobotic Technology, Inc
Street Address
1016 N. Lincoln Avenue
City
Pittsburgh
State
PA
Zip Code/Postal Code
15233-
Country
United States of America
Attention
Mr Eduardo Lugo Perez
Phone
+14126823282
Fax
+1
Email
eduardo.lugo@astrobotic.com

2. Contact Information

Same As Licensee
No
Name
Eduardo Lugo Perez
Street Address
1016 N. Lincoln Avenue
City
Pittsburgh
State
PA
Zip Code/Postal Code
15233
Country
United States of America
Phone
+14126823282
Fax
+1
Email
eduardo.lugo@astrobotic.com
Relationship
Same

Application Fees

5. Will a fee be paid?
Yes

Waivers

Type of Request
Other

STA request

13. Description
Astrobotic's Peregrine Mission 1 will deliver government and commercial science payloads and instruments to the surface of the Moon. Peregrine will be delivered to a trans lunar injection orbit on a ULA Vulcan-Centaur launch vehicle. Once separated from the Vulcan-Centaur upper stage, Peregrine's trajectory will include one elliptical loop around the Earth before intersecting the lunar orbit. After the initial highly elliptical lunar capture orbit, Peregrine will enter a lower elliptical orbit where subsystem checkouts will occur. The last orbit is a 100 km circular orbit in preparation for landing. The landing site on the Moon is in the Lacus Mortis basin and the landing coordinates are 43.91 Deg. North and 25.14 Deg. East. Peregrine's X-Band communication system will be supported during all phases of the mission by NASA's Deep Space Network (DSN). DSN will receive Telecommands from Astrobotic's Mission Control Center and deliver them to Peregrine along with ranging information using an X-Band uplink. DSN will receive Telemetry and ranging signals from Peregrine's X-Band transmitter. Peregrine's mission will last up to 57 days from launch date depending on arrival of the Moon. After landing on the Moon, Peregrine will begin its surface operations phase, providing the payloads with power and communications services for attached payloads and communications services for deployed payloads. Peregrine is designed to provide the services for one lunar day, after which time the spacecraft will shut down and arrive at End of Mission (EOM).
14. Is the Applicant filing an optional Schedule B with this application?
No

Certification

Certification Statement
No

Signature

Title
Lead RF Communications Engineer.
Signature
Eduardo Lugo Perez

Frequencies

Lower MHzUpper MHzEmissionLocation
7223.0000007233.000000
8487.0000008497.000000

Public notices

DateReportTypeServiceStatus
2021-03-19SAT01538 Action Taken Public NoticeSatellite Space Station0

Documents

DocumentTypeDateStatus
19410_SN6_FULL_PATTE.pdfForm Attachment2025-06-25Pending archive
27010_SN1_PATTERNS.pdfForm Attachment2025-06-25Pending archive
HTML.htmForm Attachment2025-06-25Pending archive
19410_SN6_FULL_PATTE.pdfForm Attachment2025-06-25Pending archive
Withdraw Receipt.htmForm Attachment2025-06-25Pending archive
Application.pdfForm Attachment2025-06-25Pending archive
19410_SN6_FULL_PATTE.pdfForm Attachment2025-06-25Pending archive
Sched S Tech Report.pdfForm Attachment2025-06-25Pending archive
Attachment Withdraw Receipt Unavailable
Attachment 19410_SN6_FULL_PATTE Unavailable
Attachment 19410_SN6_FULL_PATTE Unavailable
Attachment 19410_SN6_FULL_PATTE Unavailable
Attachment 27010_SN1_PATTERNS Unavailable
Attachment Sched S Tech Report Available
Attachment Application Available
Attachment HTML Unavailable
Attachment Annex 1 Available
Attachment ODAR Available