Intelsat IVA

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Intelsat IVA F-1
INTELSAT IVA.jpg
Start date September 26, 1975
Launcher Atlas Centaur 307
Launch site Canaveral LC-36B
Takeoff mass 1515 kg
Mass in orbit 595 kg
Manufacturer Hughes
model HS-353
lifespan 7 years
operator Intelsat
Playback information
Transponder 20 C-band
Others
Electrical power 600 W
position
drive SVM-4A with hydrazine
List of geostationary satellites

The satellites of the Intelsat IVA and Intelsat 4A series are television satellites of the International Telecommunications Satellite Consortium ( Intelsat ) based in Luxembourg . They were developed and built by the Hughes Aircraft Company based on the Intelsat IV series .

Intelsat IVA F-1

The first of six satellites was launched on September 26, 1975 with an Atlas SLV-3D Centaur-D1AR rocket from Cape Canaveral , Florida . The intended service life was seven years. The spin-stabilized satellites had a cylindrical shape, 2.38 m in diameter and 2.8 m in length, which were equipped on the outside with 17,000 solar cells for the energy supply. With the antennas that did not turn, they were about 7 m high and could transmit two television transmissions or 7250 telephone calls at the same time through the 20 transponders (16 spot and 4 wide-angle). Thanks to the improved antennas compared to the Intelsat IV generation and 20 instead of 12 transponders, the transmission capacity has almost been doubled.

Intelsat IVA F-5 and F-6

Of the six satellites, the fourth (with the designation F-5) was lost due to a leak in the engine's gas generator during take-off. The sixth satellite weighed 826 kg when launched, only about half the mass of the other satellites.

See also

Web links

Individual evidence

  1. NASA JPL: Intelsat 4A Quicklook ( Memento from January 16, 2017 in the Internet Archive )
  2. Boeing: Factsheet Intelsat IVA ( Memento from January 2, 2009 in the Internet Archive )