To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Intelsat IV F-6

From Wikipedia, the free encyclopedia

Intelsat IV F-6
Mission typeCommunications
OperatorIntelsat
COSPAR IDINT4F-6
Mission duration7 years (planned)
(Launch failure)
Spacecraft properties
BusHS-312
ManufacturerHughes Aircraft
Launch mass1,414 kilograms (3,117 lb)
BOL mass730 kilograms (1,610 lb)
Start of mission
Launch dateFebruary 20, 1975, 23:35 (1975-02-20UTC23:35Z) UTC[1]
RocketAtlas SLV-3D Centaur-D1 AR
Launch siteCape Canaveral LC-36A
Orbital parameters
Reference systemGeocentric
RegimeGeostationary
EpochPlanned
Intelsat IV
 

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.

YouTube Encyclopedic

  • 1/3
    Views:
    9 400
    75 922
    311
  • how to receive sony network on 4 feet dish antenna @asiasat7 c band Essay in urdu hindi
  • Orientar parabólica a cualquier satélite de televisión
  • Convair General Dynamics Atlas Centaur AC-62 Intelsat 5 6/9/84 Roll 1 HACL Film 00295

Transcription

History

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 17 feet (5.2 meters) 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 All seven satellites exceeded their projected life expectancies and were withdrawn from active duty, the last of which, the Intelsat IV F-1 was retired in October 1987.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.

Launch

The satellite was lost due to a launcher malfunction.[2]

See also

References

  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved April 21, 2017.
  2. ^ Ezell, Linda Neuman (1988-01-01). NASA Historical Databook. Vol. III: Programs and Projects 1969-1978. NASA. Table 4-103. Chronology of Intelsat Development and Operations, 1969-1978. NASA-SP-4012-VOL-3.


This page was last edited on 17 January 2023, at 22:13
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.