Engineering:AMOS-1 (satellite)

Short description: AMOS communications satellite

AMOS-1

Names	Affordable Modular Optimized Satellite-1 INTELSAT 24 IS-24
Mission type	Communications
Operator	Spacecom Satellite Communications (1996-2009) Intelsat (2009-2012)
COSPAR ID	1996-030B
SATCAT no.	23865
Website	https://www.amos-spacecom.com/satellites/
Mission duration	12 years (planned) 16 years (achieved)
Spacecraft properties
Spacecraft	AMOS-1
Bus	AMOS Bus
Manufacturer	Israel Aerospace Industries
Launch mass	961 kg (2,119 lb)
Dry mass	580 kg (1,280 lb)
Dimensions	2.33 m × 2.39 m × 2.07 m (7 ft 8 in × 7 ft 10 in × 6 ft 9 in) Span: 10.55 m (34.6 ft) on orbit
Power	1380 watts
Start of mission
Launch date	16 May 1996, 01:56:29 UTC
Rocket	Ariane 44L H10-3 (V86)
Launch site	Centre Spatial Guyanais, Kourou, ELA-2
Contractor	Arianespace
Entered service	1 July 1996
End of mission
Disposal	Graveyard orbit
Deactivated	July 2012
Orbital parameters
Reference system	Geocentric orbit
Regime	Geostationary orbit
Longitude	4° West (1996-2008) 47.3° East (2009-2011) 31° East (2011-2012)
Transponders
Band	7 (+ 2 spares) Ku-band
Bandwidth	72 MHz
Coverage area	Europe, Israel, Middle East
AMOS Series   Intelsat constellation

AMOS-1, then INTELSAT 24, is a commercial communications satellite which was operated by Spacecom as AMOS-1, for Affordable Modular Optimized Satellite and formed part of the AMOS series of satellites. It was the first Israeli civilian communications satellite, and was initially positioned at 4° West longitude in geostationary orbit. Then in September 2011, it was moved to 31° East.

Satellite description

Its development was based on experience from Ofeq reconnaissance satellites in association with DASA and Alcatel Espace. It was used for home television services (DTH/DBS by "Yes" company in Israel and by HBO and others in Europe). Spacecom succeeded quickly to fill all transmission abilities of AMOS-1 and accumulated additional requests. Therefore, Spacecom decided to build AMOS-2, which replaced AMOS-1 on orbit at 4° West. AMOS-1 carries nine Ku-band transponders.

Weighing 970 kg at launch, AMOS-1 incorporated a 400 newtons liquid apogee motor and fourteen reaction control thrusters, each delivering ten newtons of thrust for raising the satellite's orbit from geostationary transfer orbit (GTO) to its final geostationary orbit as well as for its attitude control. It carried 450 kg of propellant (Monomethylhydrazine and MON-3). AMOS-1 measures 10.55 m in length in its final in-orbit configuration. It is 3-axis body stabilised using Sun and Earth sensors, momentum and reaction wheels. Its solar array generates 1380 watts power, backed up by 24 A·h nickel–cadmium batteries. Cost: US$250 million. The Israeli government supports the program since 1991 with US$15 million per year.

Launch

It was launched on 16 May 1996 from Centre Spatial Guyanais, Kourou in French Guiana, aboard an Ariane 4 launch vehicle flying in the 44L configuration, which launched together with Indonesian Palapa-C2 satellite using Ariane 4's SPELDA system that can launch two satellites stacked on top of another. After its launch, it was raised to its final geostationary orbit by firing the apogee boost motor in phases. After it reached the geostationary orbit, its antennae and solar panels were deployed and the satellite was placed in its allocated slot at 4° West longitude. AMOS-1 and AMOS-2 were placed near each other to enable satellite users to aim once and reach either satellite from the same antenna. Launch was insured for over US$145 million. The satellite AMOS-1 was operational on 1 July 1996.

INTELSAT 24

In 2009, AMOS-1 was sold to Intelsat, and became INTELSAT 24 (IS-24). Intelsat moved it over the Middle East, put it into an inclined orbit to conserve fuel, and rented its capacity to Tachyon Networks for U.S. military communications.

See also

• List of Intelsat satellites
• List of satellites in geosynchronous orbit