Binariang Sdn. Bhd. of Kuala Lumpur took a major step toward enhancing Malaysia's
infrastructure and regional communications by signing a contract with Hughes Space and
Communications International, Inc. (HSCI), on 17 May 1994. The agreement concluded more
than two years of discussion following a memorandum of understanding signed in November
1991, and ended an international competition that HSCI won over three competitors. The
contract called for delivery of one Hughes HS-376
model spacecraft and an option for a second, forming the Malaysia-East Asia Satellite
(MEASAT) system. Binariang exercised its option on Nov. 30, 1994, and authorized Hughes to
proceed with a second 376 satellite.
The MEASAT system will provide the first direct-to-user (DTU) service in Malaysia, as
well as general communications services in an area reaching from India to Hawaii and from
Japan to East Australia. Among DTU services are television and educational programs beamed
to small (50-cm) home antennas. General regional communications services include
telephony, television, data transmission, and business networks. Binariang is the first
cellular operator in Malaysia to offer fully digital services.
Both MEASAT spacecraft were built by Hughes Space and Communications Company (HSC) in
El Segundo, California. The first satellite was launched aboard an Ariane-44L H10-3 rocket on Jan. 12, 1996,
from Kourou, French Guiana. Launch of the second satellite was Nov. 13, 1996, also on an Ariane-44L H10-3. HSC also supplied
equipment for a satellite control station on Malaysia's Langkawi Island and trained
Malaysian spacecraft controllers.
The MEASAT HS-376 models feature three important
performance bonuses compared to standard versions. First, each delivers 40 percent more
payload power--more than 1200 Watts--by employing gallium arsenide solar cells rather than
silicon. MEASAT 1 was the first commercial communications satellite to use gallium
arsenide solar cells. Second, HSC's lightweight, high-gain shaped antenna made its HS-376 debut on MEASAT. The antenna's specially contoured
dual surfaces and single aperture eliminate the need for multiple feedhorns. Third, MEASAT
uses a bipropellant propulsion system instead of a monopropellant for greater
stationkeeping and attitude control efficiency. MEASAT 1 is contracted to operate for 12 years; MEASAT 2 has an 11-year lifetime.
After separation from the rocket, a Thiokol Star-30
solid apogee motor lifts the spacecraft from transfer orbit to geosynchronous orbit. One
nickel-hydrogen battery supplies power during eclipses.
MEASAT 1 has five high-power Ku-band transponders, plus one spare, for DTU service.
These use 112 watt traveling-wave tube amplifiers. In addition, 12 C-band transponders
perform regional service, powered by 12 watt solid-state amplifiers, with an additional
three spare transponders. MEASAT 2 has eight 95 watt and three 62 watt Ku-band
transponders, as well as six 12 watt C-band (72 MHz) transponders, including spares.
Uplink for the C-band regional beam is 5.9 to 6.4 GHz, while downlink is 3.7 to 4.2 GHz
on both spacecraft. C-band effective isotropic radiated power (EIRP) averages 39 dBW. The
Ku-band on MEASAT 1 uses 13.25 to 14.5 GHz uplink and 10.95 to 12.4 GHz downlink. On
MEASAT 2, the uplink is 13.7 to 14.4 GHz and downlink is 10.95 to 12.62 GHz. The Ku-band
EIRP ranges from 56 to 59 dBW on MEASAT 1. The range is 55.6 to 59 dBW on MEASAT 2. Both
C-band and Ku-band use orthogonal linear polarization.
MEASAT 1 was relocated to 46° E and renamed Africasat 1 in January 2008. In early 2010 MEASAT 2 was renamed Africasat 2.
Africasat 2 was maneuvered off station in July 2018, likely to be retired.