Intelsat III F-5

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Intelsat III F-5
Mission type Communications
Operator Intelsat
COSPAR ID 1969-064A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 04051
Mission duration5 years planned
Failed to orbit
Spacecraft properties
Manufacturer TRW
Launch mass293 kilograms (646 lb)
BOL mass 151 kilograms (333 lb)
Power183 W
Start of mission
Launch dateJuly 26, 1969, 02:06 (1969-07-26UTC02:06Z) UTC [1]
Rocket Delta M
Launch site Cape Canaveral LC-17A
End of mission
DeactivatedOctober 14, 1988 (1988-10-15)
Orbital parameters
Reference system Geocentric
Regime Low Earth
Eccentricity 0.07326
Perigee altitude 252 kilometers (157 mi)
Apogee altitude 1,301 kilometers (808 mi)
Inclination 30.3°
Period 115.3 minutes
Epoch July 26, 1969
Intelsat III
 

Intelsat III F-5 was a communications satellite intended to be operated by Intelsat. Launched towards geostationary orbit in 1969 it failed to achieve orbit.

Contents

Design

The fifth of eight Intelsat III satellites to be launched, Intelsat III F-5 was built by TRW. It was a 293-kilogram (646 lb) spacecraft equipped with two transponders to be powered by body-mounted solar cells generating 183 watts of power. [2] It had a design life of five years and carried an SVM-2 apogee motor for propulsion. [3]

Launch

Intelsat III F-5 was launched by a Delta M rocket, flying from Launch Complex 17A at the Cape Canaveral Air Force Station. The launch took place on July 26, 1969, with the spacecraft bound for a geosynchronous transfer orbit. [1]

Due to a failure in the third phase of the launch process, the satellite did not reach the desired orbit.

See also

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References

  1. 1 2 McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved April 21, 2017.
  2. Wade, Mark. "Intelsat 3". Encyclopedia Astronautica. Archived from the original on February 23, 2002. Retrieved April 21, 2017.
  3. Krebs, Gunter. "Intelsat-3". Gunter's Space Page. Retrieved April 21, 2017.