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| disposal_type = Decommissioned
| disposal_type = Decommissioned
| deactivated = {{end-date|12 June 1968}}<ref>{{cite web|url=http://science1.nasa.gov/missions/essa/|title=ESSA|publisher=NASA Science|accessdate=8 December 2013}}</ref>
| deactivated = {{end-date|12 June 1968}}<ref>{{cite web|url=http://science1.nasa.gov/missions/essa/|title=ESSA|publisher=NASA Science|accessdate=8 December 2013|deadurl=yes|archiveurl=https://web.archive.org/web/20131211172641/http://science1.nasa.gov/missions/essa/|archivedate=11 December 2013|df=}}</ref>
| decay_date =
| decay_date =



Revision as of 15:13, 29 January 2018

ESSA-1
ESSA 1
Mission typeWeather satellite
OperatorESSA/NASA
COSPAR ID1966-008A Edit this at Wikidata
SATCAT no.1982
Spacecraft properties
ManufacturerRCA Astro
Launch mass304 kilograms (670 lb)[1]
Start of mission
Launch date3 February 1966, 07:41:23 (1966-02-03UTC07:41:23Z) UTC[2]
RocketDelta C
Launch siteCape Canaveral LC-17A
End of mission
DisposalDecommissioned
Deactivated12 June 1968 (1968-06-13)[3]
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis7,115.60 kilometers (4,421.43 mi)
Eccentricity0.0083082
Perigee altitude685 kilometers (426 mi)
Apogee altitude803 kilometers (499 mi)
Inclination97.94 degrees
Period99.56 minutes
Epoch7 December 2013, 20:11:52 UTC[4]

ESSA-1 (or OT-3) was a spin-stabilized operational meteorological satellite. Its name was derived from that of its oversight agency, the Environmental Science Services Administration (ESSA).

Launch

ESSA-1 was launched on 3 February 1966 at 07:41 UTC. It was launched atop a Delta rocket from Cape Canaveral, Florida. The spacecraft had a mass of 304 kilograms (670 lb) at the time of launch. ESSA-1 had an inclination of 97.91°, and an orbited the earth once every 100 minutes. Its perigee was 702 kilometers (379 nmi) and its apogee was 845 kilometers (456 nmi).

ESSA-1 had a similar design to that of the TIROS satellite series. It was an 18-sided right prism, measuring 107 centimeters (42 in) across opposite corners and 56 centimeters (22 in). It had a reinforced baseplate, which carried most of the subsystems and a cover assembly (hat). ESSA-1 had approximately 10,000 1-cm by 2-cm solar cells, which charged 21 nickel–cadmium batteries. ESSA-1 was designed to take pictures of daytime cloud cover, record them, and transmit them when it was in range of a ground acquisition station.

The satellite spin rate and attitude were determined primarily by a magnetic attitude spin coil (MASC). The MASC was a current-carrying coil mounted in the cover assembly. The magnetic field induced by the coil interacted with that of the Earth's magnetic field, and provided the necessary torque to maintain a desired spin rate of 9.225 revolutions per minute (rpm). Five small solid-fuel thrusters mounted on the baseplate provided a secondary means of controlling the spin rate.

ESSA-1 operated normally until 6 October 1966, when the camera system failed. The spacecraft was fully deactivated on 8 May 1967, after being left on for an additional period of time for engineering purposes.

References

  1. ^ "ESSA 1". National Space Science Data Center. Retrieved 8 December 2013.
  2. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 8 December 2013.
  3. ^ "ESSA". NASA Science. Archived from the original on 11 December 2013. Retrieved 8 December 2013. {{cite web}}: Unknown parameter |deadurl= ignored (|url-status= suggested) (help)
  4. ^ "ESSA 1 (OT-3) Satellite details 1966-008A NORAD 1982". N2YO. 7 December 2013. Retrieved 8 December 2013.

Public Domain This article incorporates public domain material from ESSA 1. National Aeronautics and Space Administration. Retrieved 2009-03-05.