OPS 5113
{{short description|American navigation satellite}}
{{Use American English|date=March 2014}}
{{Use dmy dates|date=November 2020}}
{{Infobox spaceflight
| name = OPS 5113
| names_list = Navstar 3
GPS I-3
GPS SVN-3
| image =
| image_caption =
| image_size = 290px
| mission_type = Navigation
Technology
| operator = U.S. Air Force
| SATCAT = 11054
| mission_duration = 5 years (planned)
{{frac|13|1|2}} years (achieved)
| spacecraft = Navstar
| spacecraft_type = GPS Block I
| manufacturer = Rockwell Space Systems
| launch_mass = {{cvt|758|kg}}
| dimensions = 5.3 meters of long
| power = 400 watts
| launch_date = 7 October 1978, 00:28:00 UTC
| launch_rocket = Atlas F / SGS-1
(Atlas-47F)
| launch_site = Vandenberg, SLC-3E
| launch_contractor = Convair
General Dynamics
| entered_service = 13 November 1978
| deactivated = 18 May 1992
| orbit_reference = Geocentric orbit{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1978-093A|title=Trajectory: Navstar 3 1978-093A|publisher=NASA|date=14 May 2020|access-date=21 November 2020}} {{PD-notice}}
| orbit_regime = Medium Earth orbit
(Semi-synchronous)
| orbit_slot =
| orbit_periapsis = {{cvt|20285|km}}
| orbit_apoapsis = {{cvt|20312|km}}
| orbit_inclination = 62.80°
| orbit_period = 722.60 minutes
| apsis = gee
| programme = Global Positioning System
| previous_mission = OPS 5112 (Navstar 2)
| next_mission = OPS 5114 (Navstar 4)
}}
OPS 5113, also known as Navstar 3, GPS I-3 and GPS SVN-3, was an American navigation satellite launched in 1978 as part of the Global Positioning System development programme. It was the third of eleven Block I GPS satellites to be launched.
Background
Global Positioning System (GPS) was developed by the U.S. Department of Defense to provide all-weather round-the-clock navigation capabilities for military ground, sea, and air forces. Since its implementation, GPS has also become an integral asset in numerous civilian applications and industries around the globe, including recreational used (e.g., boating, aircraft, hiking), corporate vehicle fleet tracking, and surveying. GPS employs 24 spacecraft in 20,200 km circular orbits inclined at 55°. These vehicles are placed in 6 orbit planes with four operational satellites in each plane.{{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1978-093A|title=Display: Navstar 3 1978-093A|publisher=NASA|date=14 May 2020|access-date=21 November 2020}} {{PD-notice}}
Spacecraft
The first eleven spacecraft (GPS Block 1) were used to demonstrate the feasibility of the GPS system. They were 3-axis stabilized, nadir pointing using reaction wheels. Dual solar arrays supplied over 400 watts. They had S-band communications for control and telemetry and Ultra high frequency (UHF) cross-link between spacecraft. They were manufactured by Rockwell Space Systems, were 5.3 m across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block 1 spacecraft were inclined at 63°.
Launch
OPS 5113 was launched at 00:28 UTC on 7 October 1978, atop an Atlas F launch vehicle with an SGS-1 upper stage. The Atlas used had the serial number 47F, and was originally built as an Atlas F.{{cite web|url=http://planet4589.org/space/log/launchlog.txt|title=Launch Log|publisher=Jonathan's Space Report|first=Jonathan|last=McDowell|access-date=12 July 2012}} The launch took place from Space Launch Complex 3E at Vandenberg Air Force Base,{{cite web|url=http://planet4589.org/space/lvdb/list2.html|title=Launch List|publisher=Jonathan's Space Report|work=Launch Vehicle Database|first=Jonathan|last=McDowell|access-date=12 July 2012|archive-date=15 August 2020|archive-url=https://web.archive.org/web/20200815040340/http://planet4589.org/space/lvdb/list2.html|url-status=dead}} and placed OPS 5113 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-27 apogee motor.{{cite web |url=http://space.skyrocket.de/doc_sdat/navstar.htm|title=GPS (Navstar)|first=Gunter|last=Krebs|publisher=Gunter's Space Page|access-date=12 July 2012}}
Mission
By 13 November 1978, OPS 5113 was in an orbit with a perigee of {{cvt|20285|km}}, an apogee of {{cvt|20312|km}}, a period of 722.60 minutes, and 62.80° of inclination to the equator.{{cite web|url=http://planet4589.org/space/log/satcat.txt|title=Satellite Catalog|publisher=Jonathan's Space Report|first=Jonathan|last=McDowell |access-date=12 July 2012}} The satellite had a design life of 5 years and a mass of {{cvt|758|kg}}. It broadcast the PRN 06 signal in the GPS demonstration constellation, and was retired from service on 18 May 1992.
See also
{{Portal|Spaceflight}}
References
{{Reflist|30em}}
{{GPS satellites}}
{{Orbital launches in 1978}}