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Azerspace/africasat-1a – Orbital Azerspace/Africasat-1a User Manual

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Dulles, Virginia 20166

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©2014 Orbital Sciences Corporation

FS005_10_2998

Coverage Contour Maps

Ku-band EIRP Contours – 11.2 GHz

East (Central Asia)

West (Europe)

Ku-band G/T Contours – 14.0 GHz

East (Central Asia)

West (Europe)

C-band EIRP Contours – 3,740 MHz

Africa and Europe

Central Asia and Europe

C-band G/T Contours – 5,965 MHz

Africa and Europe

Central Asia and Europe

Azerspace/Africasat-1a

Specifications

Spacecraft

Launch Mass:

3,275 kg (7,220 lb.)

Solar Arrays:

Four panels per array, UTJ Gallium
Arsenide cells

Stabilization:

3-axis stabilized; zero momentum system

Propulsion:

Liquid bi-propellant transfer orbit system;
monopropellant (hydrazine) on-orbit system

Batteries:

Two >4840 W-Hr capacity Li-Ion batteries

Mission Life:

15 years

Orbit: 46

°

East Longitude

Hybrid Payload

C-band
Repeater:

24 active transponders

Antenna:

2.5 x 2.7 m single shell super-elliptical
deployable reflector; 1.4 x 1.4 m single shell
super-elliptical deck-mounted

Ku-band
Repeater:

12 active transponders

Antenna:

2.5 x 2.7 m single shell super-elliptical
deployable reflector

Launch

Launch Vehicle:

Ariane 5

Site:

Kourou, French Guiana

Date:

February 7, 2013

Mission Partners

Azercosmos OJSCo.

Orbital Sciences Corporation

Prime Contractor for the Azersapce/Africasat-1a spacecraft and
ground system