TIROS-9

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TIROS-9
TIROS IX Spac0021-repair.jpg
TIROS-9 satellite
Mission type Weather satellite
Operator NASA
COSPAR ID 1965-004A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 978
Spacecraft properties
Spacecraft type TIROS
Manufacturer RCA  / GSFC
Launch mass138.30 kilograms (304.9 lb) [1]
Dimensions1.07 m × 0.56 m (3.5 ft × 1.8 ft)
Start of mission
Launch dateJanuary 22, 1965, 07:52 (1965-01-22UTC07:52Z) UTC [2]
Rocket Thor-Delta C 374/D-28
Launch site Cape Canaveral LC-17A
End of mission
Last contactFebruary 15, 1967 (1967-02-16)
Orbital parameters
Reference system Geocentric
Regime Low Earth
Eccentricity 0.11693 [1]
Perigee altitude 705 kilometers (438 mi) [1]
Apogee altitude 2,582 kilometers (1,604 mi) [1]
Inclination 96.43° [1]
Period 119.23 minutes [1]
Epoch January 22, 1965 [1]
Instruments
Television Camera System
  TIROS-8
TIROS-10  

TIROS-9 (also called TIROS-I or A-54) was a spin-stabilized meteorological satellite. It was the ninth in a series of Television Infrared Observation Satellites.

Contents

Launch

TIROS-9 was launched on January 22, 1965, by a Thor-Delta rocket from Cape Canaveral Air Force Station, Florida. The spacecraft functioned nominally until February 15, 1967. The satellite orbited the Earth once every 2 hours, at an inclination of 96°. Its perigee was 705 kilometers (438 mi) and apogee was 2,582 kilometers (1,604 mi). [1]

Mission

TIROS-9 was a spin-stabilized meteorological spacecraft designed to test experimental television techniques and infrared equipment. The satellite was in the form of an 18-sided right prism, 107 cm in diameter and 56 cm high. The top and sides of the spacecraft were covered with approximately 9000 1-by 2-cm silicon solar cells. It was equipped with 2 independent television camera subsystems for taking cloudcover pictures, plus an omnidirectional radiometer and a five-channel scanning radiometer for measuring radiation from the earth and its atmosphere. The satellite spin rate was maintained between 8 and 12 rpm by use of five diametrically opposed pairs of small, solid-fuel thrusters.

The TV system operated normally until April 1, 1965, when one of the wide-angle TV cameras failed. The other camera operated normally until July 26, 1965, and sporadically until February 15, 1967. TIROS 9 was the first satellite in the TIROS series to be placed in a near-polar orbit, thereby increasing TV coverage to the entire daylight portion of the Earth. [3]

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References

  1. 1 2 3 4 5 6 7 8 "TIROS 9". National Space Science Data Center Master Catalog. NASA Goddard Space Flight Center. Retrieved June 4, 2018.
  2. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved June 4, 2018.
  3. "TIROS 9 (1965-004A)". NASA Goddard Space Flight Center. Retrieved June 4, 2018.PD-icon.svg This article incorporates text from this source, which is in the public domain .