ESSA-9

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ESSA-9
ESSA-9.jpg
ESSA-9 being checked out before launch
Mission typeMeteorology
OperatorESSA (1969-70)
NOAA (1970-72)
COSPAR ID1969-016A
SATCAT no.3764
Mission duration1,726 days[1]
Spacecraft properties
Launch mass145 kilograms (320 lb)
Start of mission
Launch dateFebruary 26, 1969, 07:47:01 (1969-02-26UTC07:47:01Z) UTC[2]
RocketDelta E1
Launch siteCape Canaveral LC-17B
End of mission
DisposalDecommissioned
DeactivatedNovember 1972 (1972-12)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis7,843.18 kilometers (4,873.53 mi)
Eccentricity0.00508
Perigee1,432 kilometers (890 mi)
Apogee1,512 kilometers (940 mi)
Inclination101.99 degrees
Period115.21 minutes
Mean motion12.49
EpochDecember 7, 2013, 20:28:49 UTC[3]
Instruments
Advanced Vidicon Camera System (AVCS), Flat Plate Radiometer (FPR)[4]

ESSA-9, also known as TOS-G, was a meteorological satellite.[5] Its name was derived from that of its oversight agency, the Environmental Science Services Administration (ESSA). ESSA-9 replaced the ESSA-7 satellite.

Launch and orbit[edit]

ESSA-9 was launched on a three-stage Delta rocket from Cape Canaveral, Florida. The launch occurred at 07:47 UTC (02:47 EDT) on February 26, 1969. The spacecraft was placed in a sun-synchronous orbit of 101.4° inclination. Immediately after launch ESSA-9 had a perigee of 1,427.0 kilometers (886.7 mi) and an apogee of 1,508.0 kilometers (937.0 mi), giving it an orbital period of 115.2 minutes, or a mean motion of 12.5 orbits per day.[2] ESSA-9 operated for 1,726 days before it was deactivated in November 1972.

Spacecraft[edit]

The ESSA-9 spacecraft was similar to the TIROS series of satellites, having an 18-sided polygonal shape that measured 42 inches (110 cm) in diameter and 22 inches (56 cm) high. It weighed 320 pounds (150 kg). The body of ESSA-9 was made of aluminum alloy and stainless steel. The shell of the craft was covered with 10,020 solar cells.[1] The solar cells recharged the 63 nickel–cadmium batteries during the time the spacecraft was in sunlight.[1] ESSA-9 employed the same cartwheel-style stabilization as the TIROS-9 satellite. The satellite used a magnetic attitude spin coil (MASC) to control its attitude while in orbit. The magnetic field induced by the MASC's current interacted with the earth's magnetic field to provide the torque necessary to maintain a desired spin rate of 9.225 rpm.[6]

Instruments[edit]

ESSA-9 carried two sets of two main instruments, the Advanced Vidicon Camera System (AVCS) and the Flat Plate Radiometer (FPR). The AVCS was used to collect imagery of cloud cover on earth. The cameras had a resolution of 2 miles (3.2 km) and covered an area of 2,000 square miles (5,200 km2). The cameras took single images of a particular region of the earth's surface once a day. The FPR's were used to measure the global distribution of solar radiation reflected by the earth and the earth's atmosphere. They also measured long-wave emissions from the earth. The sensors used in the ESSA satellites were from the earlier Nimbus program.

References[edit]

  1. ^ a b c NASA Science page Archived August 25, 2009, at the Wayback Machine., ESSA-9
  2. ^ a b Launch info
  3. ^ "ESSA 9 (TOS-G) Satellite details 1969-016A NORAD 3764". N2YO. December 7, 2013. Retrieved December 8, 2013.
  4. ^ Experiments on ESSA-9
  5. ^ tbs-satellite.com Satellit Fact Sheet: ESSA-9
  6. ^ Spacecraft details

External links[edit]