Amazonas 4A
Names | Amazonas 4A, Amazonas 4 |
---|---|
Operator | Hispasat |
COSPAR ID | 2014-011A |
SATCAT no. | 39616![]() |
Mission duration | 15 years |
Spacecraft properties | |
Bus | GEOStar-2 |
Manufacturer | Orbital Sciences Corporation |
Launch mass | 2,938 kg |
Dry mass | 1,241 kg |
Start of mission | |
Rocket | Ariane 5 ECA |
Launch site | Kourou Space Center |
Orbital parameters | |
Longitude | 73.9º W |
Semi-major axis | 42,164 km |
Periapsis altitude | 35,780.1 km |
Apoapsis altitude | 35,807.6 km |
Inclination | 0.1º |
Period | 1,436.1 minutes |
Payload | |
24 Ku-band transponders | |
Amazonas 4 network |
The Amazonas 4A, renamed in 2016 Amazonas 4 and since 2017 known as the Hispasat 74W-1, is a Spanish commercial communications satellite developed by Orbital Sciences Corporation and operated by Hispasat. It was successfully launched in 2014 and it is expected to have a service life of 15 years however, shortly after its launch the satellite suffered a power failure that limited its operability and life.[1] It is positioned to cover all of South America and during its service life the satellite has offered coverage for some important events such as the 2016 Summer Olympics and World Cup football broadcasts.[2][3]
Body[]
The satellite is based on the GEO Star-2.4 bus and has a dry mass of 1,241 kg. It is shaped like a square-faced prism 5 meters tall. Its lateral faces hold two deployable reflector-antennas and two retracting solar panels that, when fully deployed, give the satellite a diameter nearing 23 meters.[4] At launch, its mass was increased to 2,938 kg.[5]
Propulsion[]
The main engine is the bipropellant BT-4 developed by the Japanese company IHI Aerospace. It is fueled by Unsymmetrical Dimethylhydrazine using Nitrogen Tetroxide as the oxidizer.The fuel is stored in spherical tanks pressurized with Helium.
The engine alone is 0.65 meters tall and has a dry mass of 4 kg while capable of producing 450 N of thurst.[6]
Attitude Determination & Control Subsystem[]
The attitude and control subsystem is state of the art employing a combination of electrically powered set of reaction wheels and chemical-inertial Hydrazine monopropellant thrusters in order to provide precise Earth-pointing capabilities.
Electrical Power Subsystem[]
The power requirements of the satellite are up to 4.8 kW although it was projected to support up to 6.2 kW. Those are provided by a combination of two independent arrays each composed by four panels featuring Ultra-Triple-Junction GaAs Solar cells and two 5,053 Watt-Hour Li-Ion batteries and avionics for power storage and distribution.
Communications Subsystem[]
The communications subsystem is the main payload of the satellite. It consists on 24 Ku-band transponders subdivided in two 15-for-12 groups of Linearized Channel Travelling Wave Tube Amplifiers (LCTWTAs).[7] In addition to two 2.5 x 2.7 meter single shell super elliptical deployable reflectors. All of them orientable and capable of working individually or grouped in order to speed up or relay communications. Nonetheless, a power failure in the electrical subsystem provoked the quick degradation of the subsystem and it has been speculated that, as a result, the satellite lost almost half of its communication potential being able to maintain only 12 of its transponders operational. In conjunction to the natural degradation of the solar panels in space, has greatly shortened the satellite's service life and its utility.
It's design signal strength lies between 46 and 48.5 dBW throughout all of South America.[8]
Launch[]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/2/24/Ariane_5_Mission_21.jpg/172px-Ariane_5_Mission_21.jpg)
The satellite was launched the 22nd of March 2014, at 22:04 UTC, via an Ariane 5 ECA vehicle, from the Guiana Space Center in Kourou, French Guiana.[9] The launch was shared with the Astra 5B satellite.[10][11] Amazonas 4A was successfully put into a GEO orbit of 35,807.6 km of apogee and 35,780.1 km of perigee, an inclination of 0.1º, a period of 1,436.1 minutes and a semi major maxis of 42,164 km. Since it was designed to cover all of South America, it initially operated on the longitude 61º W but since 2017 it has shifted to 73.9º W.[12][13][14][15]
Power failure[]
Shortly after reaching its intended orbit the satellite suffered a partial power failure losing some of its capabilities and shortening its operational life.
The loss was estimated to halve the satellite's capabilities.[16] However, the difficulty in assessing the causes and severity of the failure forced Hispasat and the insurance company to open a joint investigation. It will remain open until the loss of the satellite, scheduled for 2029, but so far, the insured value has been estimated at 145 million euros.[17][18] The economic impact of the power failure has been estimated on 11 million euros of lost income during for the first quarter of 2014 for Hispasat, with further 5.4 million euros lost in operating income.[19]
In addition, the incident provoked the scrapping of the high power companion satellite, the Amazonas 4B, replaced by the future Amazonas 5 and the two renamings the satellite has undergone.[20][21]
See also[]
References[]
- ^ Satélite Amazonas 4A, retrieved 2021-07-10
- ^ "Technical details for satellite AMAZONAS 4A". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2021-07-06.
- ^ "Amazonas 4A readies for World Cup". advanced-television.com. Retrieved 2021-07-15.
- ^ "Orbital-Built Amazonas 4A Commercial Communications Satellite Successfully Launched". Northrop Grumman Newsroom. Retrieved 2021-07-06.
- ^ "Hispasat 74W-1". www.hispasat.com (in Spanish). Retrieved 2021-08-18.
- ^ "Amazonas 4A – Spacecraft & Satellites". Retrieved 2021-07-06.
- ^ Robbins, Neal; Eze, David; Cohen, Helen; Zhai, Xiaoling; McGeary, William; Menninger, William; Chen, Morgan; Rodgers, Eddie (2018). "Space Qualified 200-Watt Q-band Linearized Traveling-Wave Tube Amplifier" (PDF). NASA. Archived (PDF) from the original on 2021-07-12.
- ^ "Amazonas 4A → Amazonas 4 → Hispasat 74W-1". Gunter's Space Page. Retrieved 2021-07-06.
- ^ "HISPASAT chooses Arianespace to launch its Amazonas 4A and AG1 satellites". Arianespace. Retrieved 2021-07-06.
- ^ "Orbital-Built Amazonas 4A Commercial Communications Satellite Ready for Launch". www.businesswire.com. 2014-03-20. Retrieved 2021-07-10.
- ^ "Ariane 5 Successfully Launches Astra 5B and Amazonas 4A Satellites". AmericaSpace. 2014-03-22. Retrieved 2021-07-10.
- ^ "Real time satellite tracking for: AMAZONAS 4A". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2021-07-15.
- ^ "Hispasat 74W-1 at 73.9°W - LyngSat". www.lyngsat.com. Retrieved 2021-08-18.
- ^ "El satélite Amazonas 4 de HISPASAT completa el traslado a su nueva posición orbital en 74º Oeste". Hispaviación (in Spanish). 2017-12-21. Retrieved 2021-08-19.
- ^ "El satélite Amazonas 4 cambia de posición y ofrecerá nuevos servicios sobre Brasil y Sudamérica". Avion Revue Internacional (in Spanish). 2017-12-21. Retrieved 2021-08-19.
- ^ "Amazonas-4 major failure". advanced-television.com. Retrieved 2021-07-11.
- ^ "Power System Failure Expected To Cost Amazonas 4A Half its Capacity, Prompt $100M Insurance Claim". SpaceNews. 2014. Retrieved 2021-07-10.
{{cite web}}
: CS1 maint: url-status (link) - ^ Forrester, Chris. "Hispasat's $100m claim on Amazonas 4A". advanced-television.com. Retrieved 2021-07-15.
- ^ "Spaceflight Now | Breaking News | Power system failure detected on Amazonas 4A". www.spaceflightnow.com. Retrieved 2021-07-10.
- ^ "Amazonas 4B". Gunter's Space Page. Retrieved 2021-07-11.
- ^ "Hispasat". www.hispasat.com (in Spanish). Retrieved 2021-07-11.
- Satellites in geostationary orbit
- Satellites of Spain