ESSA-9

From Wikipedia, the free encyclopedia
Jump to: navigation, search
ESSA-9
ESSA-9.jpg
ESSA-9 being checked out before launch
Mission type Meteorology
Operator ESSA (1969-70)
NOAA (1970-72)
COSPAR ID 1969-016A
SATCAT № 3764
Mission duration 1,726 days[1]
Spacecraft properties
Launch mass 145 kilograms (320 lb)
Start of mission
Launch date 26 February 1969, 07:47:01 (1969-02-26UTC07:47:01Z) UTC[2]
Rocket Delta E1
Launch site Cape Canaveral LC-17B
End of mission
Disposal Decommissioned
Deactivated November 1972 (1972-12)
Orbital parameters
Reference system Geocentric
Regime Low Earth
Semi-major axis 7,843.18 kilometers (4,873.53 mi)
Eccentricity 0.00508
Perigee 1,432 kilometers (890 mi)
Apogee 1,512 kilometers (940 mi)
Inclination 101.99 degrees
Period 115.21 minutes
Mean motion 12.49
Epoch 7 December 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] ESSA-9 replaced the ESSA-7 satellite.

Launch & orbit[edit]

The 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 26 February 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]

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 the 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] The 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]

The 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 would take 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.

ESSA-9 is launched aboard a Delta E1 rocket in 1969

References[edit]

External links[edit]