Azerspace/africasat-1a – Orbital Azerspace/Africasat-1a User Manual
Page 2

Orbital Sciences Corporation
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Dulles, Virginia 20166
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www.orbital.com
©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