| Intelsat IV F-6 | |
| Mission Type: | Communications |
| Operator: | Intelsat |
| Cospar Id: | INT4F-6 |
| Mission Duration: | 7 years (planned) (Launch failure) |
| Spacecraft Bus: | HS-312 |
| Manufacturer: | Hughes Aircraft |
| Bol Mass: | 730kg (1,610lb) |
| Launch Mass: | 1414kg (3,117lb) |
| Launch Date: | UTC[1] |
| Launch Rocket: | Atlas SLV-3D Centaur-D1 AR |
| Launch Site: | Cape Canaveral LC-36A |
| Orbit Epoch: | Planned |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Geostationary |
| Apsis: | gee |
| Programme: | Intelsat IV |
| Previous Mission: | Intelsat IV F-5 |
| Next Mission: | Intelsat IV F-7 |
Intelsat IV F-6 was a geostationary communication satellite built by Hughes, it was owned by Intelsat. The satellite was based on the HS-312 platform and its estimated useful life was 7 years.
The Intelsat IV F-6 was part of the Intelsat IV series which consisted of eight communications satellites, launched from Cape Canaveral during the early 1970s, marked the fifth generation of geostationary communications satellites developed by the Hughes Aircraft Company since 1963 with the launch of Syncom II, the world's first synchronous satellite. The Syncom II was 15 cm high and 28 inches in diameter, weighing 78 pounds in orbit. In contrast, the Intelsat IVs weighed more than £ 1,300 (595 kg) into orbit and were more than 17abbr=offNaNabbr=off in diameter. All seven satellites exceeded their projected life expectancies and were withdrawn from active duty, the last of which, the Intelsat IV F-1 was retired in October 1987.
The satellite was equipped with 12 C-band transponders. It had 6,000 two-way relay phone calls or broadcast 12 concurrent color television programs or mixed combinations of communications traffic including data and fax.
The satellite had 12 channels of broadband communication. Each channel had a bandwidth of 40 MHz and provided about 500 communication circuits.
The satellite was lost due to a launcher malfunction.[2]