Today we are going to address a very important topic, INSAT-3A, which has become relevant in different aspects of daily life. This issue has aroused the interest of many people and has generated an intense debate in society in general. INSAT-3A is a topic that has been the subject of study, reflection and analysis by experts in various disciplines, who have dedicated time and effort to understanding its implications and consequences. Throughout this article, we will explore different perspectives on INSAT-3A, examine its impact in different areas, and discuss possible solutions or approaches to effectively address this issue.
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Mission type | Communications Weather |
---|---|
Operator | INSAT |
COSPAR ID | 2003-013A |
SATCAT no. | 27714 |
Website | INSAT 3A |
Spacecraft properties | |
Manufacturer | ISRO |
Launch mass | 2,950 kilograms (6,500 lb) |
Dimensions | 2.8 x 1.7 x 2.0 metres |
Power | 3.1 kilowatts |
Start of mission | |
Launch date | 9 April 2003, 22:52 | UTC
Rocket | Ariane 5G V160 |
Launch site | Kourou ELA-3 |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 93.5° East (0°00′N 93°30′E / 0°N +93.5°E) |
Inclination | 74 degrees |
Period | 12 years |
INSAT-3A, a multipurpose satellite built by ISRO was launched by Ariane in April 2003. It is located at 93.5 degree East longitude. It is third satellite in INSAT-3 series after INSAT-3B & INSAT-3C. Built at a cost of $53 mn, it provides communication, weather, and search and rescue services.
INSAT 3A was launched by Ariane-5 launch vehicle of Arianespace on April 9, 2003, at 22.52 UTC from Kourou, French Guiana.[1] It was placed into a Geosynchronous Transfer Orbit (GTO), 30 minutes after the lift-off in 3-axis stabilized mode, with a perigee (nearest point to earth) of 859 km and an apogee (farthest point to earth) of 36,055 km and an inclination of 1.99 degrees with respect to the equator.[2] Its co-passenger on its launch was GALAXI-XII of PanAmSat. Its Master Control Facility (MCF) is located at Hassan, Karnataka (India). It is 3-axis body stabilised in orbit using momentum and reaction wheels, solar flaps, magnetic torquers and eight 10 N and eight 22 N reaction control thrusters. Its propulsion system consists of 440 N Liquid Apogee Motor MON-3 (Mixed Oxides of Nitrogen) and MMH (MonoMethylHydrazine) for orbit raising.
The satellite raised its orbit to GEO and arrived in the 93.5 degree East longitude orbital location.[3] It joined INSAT-3B and INSAT-3C which were already in orbit operating from a similar orbital location.[4]
The INSAT-3A communications payload consists of:[5]
The INSAT-3A meteorological payload consists of[5]