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IAI AMOS-1

Spacecraft and Launch Vehicles

AMOS-1, later renamed Intelsat 24, was the first Israeli civilian communications satellite. The name stands for Affordable Modular Optimized Satellite. It was developed by Israel Aircraft Industries, now Israel Aerospace Industries, with assistance from DASA and Alcatel Espace, for the operator Spacecom, and drew on the experience gained with the Ofeq reconnaissance satellites. It was launched on 16 May 1996 from Kourou in French Guiana on an Ariane 4 in the 44L configuration, sharing the flight with the Indonesian Palapa-C2, and weighed roughly 970 kg at launch with nine Ku-band transponders. It served home television customers from 4 degrees west until AMOS-2 replaced it, and in 2009 it was sold to Intelsat and became Intelsat 24.

Facts
Year
1996 1
Propulsion
MMH and MON-3 (hypergolic) 2
Engine Class
Rocket 2
Engine
400 N liquid apogee motor with fourteen 10 N reaction control thrusters 2
Comparison
Body Style
Spacecraft 1
Connections

Exemplifies

Source AMOS-1 (satellite) (Wikipedia)

Of Make

Source Encyclopedia Astronautica: AMOS 1
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Gunter's Space Page: AMOS 1 Intelsat 24Entry text, developer
Quote, Entry text, developer
communications satellite was developed by Israel Aircraft Industries

Originated In

Also in Geography Atlas: where this subject originated.

Source Gunter's Space Page: AMOS 1 Intelsat 24Entry text, Israeli satellite
Quote, Entry text, Israeli satellite
The Israeli AMOS 1 (Affordable Modular Optimized Satellite) communications satellite
Sources
1. Encyclopedia Astronautica: AMOS 1
Encyclopedia Astronautica
  • Entry text, launch year
    Launched 1996.
  • Entry text, satellite
    Communication satellite built by IAI for Spacecom Ltd., Israel.
  • Of Make: Israel Aerospace Industries, Entry text, builder
    Communication satellite built by IAI for Spacecom Ltd., Israel.
View the Source
2. AMOS-1 (satellite) (Wikipedia)
  • Satellite description, propellant
    It carried 450 kg of propellant (Monomethylhydrazine and MON-3).
  • Satellite description, apogee motor
    AMOS-1 incorporated a 400 newtons liquid apogee motor
  • Satellite description, engine fitted
    AMOS-1 incorporated a 400 newtons liquid apogee motor and fourteen reaction control thrusters
  • Exemplifies: Orbital Spaceflight, Launch, orbit
    After its launch, it was raised to its final geostationary orbit by firing the apogee boost motor in phases.
View the Source
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